Mir home
topic index

Mission Control
Credit - © Mark Wade

Program: Mir. Objective: Manned. Type: Space station. The Mir space station was the last remnant of the once mighty Soviet space programme. It was built to last only five years, and was to have been composed of modules launched by Proton and Buran/Energia launch vehicles. These modules were derived from those originally designed by Chelomei in the 1960's for the Almaz military station programme. As the Soviet Union collapsed Mir stayed in orbit, but the final modules were years late and could only be completed with American financial assistance. Kept flying over a decade beyond its rated life, Mir proved a source of pride to the Russian people and proved the ability of their cosmonauts and engineers to improvise and keep operations going despite all manner of challenges and mishaps.

The design of an improved model of the Salyut DOS-17K space station was authorised as part of the third generation of Soviet space systems in a 17 February 1976 decree. At that time it was planned that the two stations (DOS-7 and DOS-8) would be equipped with two docking ports at either end of the station and an additional two ports at the sides of the forward small diameter compartment. By the time of the draft project in August 1978 this had evolved to the final Mir configuration of one aft port and five ports in a spherical compartment at the forward end of the station. Up to that time it was planned that the ports would provide docking positions for 7 tonne modules derived from the Soyuz spacecraft. These would use the Soyuz propulsion module, as in Soyuz and Progress, but would be equipped with long laboratory modules in place of the descent module and orbital module.

Following the decision to cancel Chelomei's manned Almaz military space station programme, a resolution of February 1979 consolidated the programs, with the docking ports to be reinforced to accommodate 20 tonne space station modules based on Chelomei's TKS manned ferry spacecraft. This order was unpopular with NPO Energia engineers, who felt that often-replaced lower-cost 7 tonne modules were a better technical solution. Nevertheless NPO Energia was made responsible for the overall space station, but subcontracted the work to KB Salyut due to the press of in-house work on Energia, Salyut 7, Soyuz-T, and Progress. The subcontractor began work in the summer of 1979, with drawings being released in 1982-1983. New systems incorporated into the station included the Salyut 5B digital flight control computer and gyrodyne flywheels (taken from Almaz), and the new Kurs automatic rendezvous system, Altair satellite communications system, Elektron oxygen generators, and Vozdukh carbon dioxide scrubbers. Mir was part of the Kosmometriy scientific program, with the objective of measuring the precise distance and characteristics of the earth's surface, ocean, and atmosphere, including spectral characterisation.

By early 1984 all work on Mir ground to a halt as all resources were put on getting the Buran space shuttle into flight test. This changed in the spring 1984 when Glushko was called into the office of the Central Committee's Secretary for Space and Defence and ordered to orbit Mir by the 27th Communist Party Congress in the spring of 1986. By the end of 1984 the static and dynamic test models of the station had been completed. The ground test model of the station was delivered in December 1984. The use of this full-fidelity test article, an approach taken on the Almaz program, was new to the civilian DOS project.

A major problem was that the station ended up one tonne heavier than designed due to the final weight of the electrical cabling Even after removing most of the experimental equipment (it would have to be delivered to the station later by ferry craft) it still exceeded the performance of the Proton booster to the planned 65 degree inclination orbit. The decision was finally taken in January 1985 to use the same 51.6 degree orbit as Salyut, although this would reduce photographic coverage of the Soviet Union. Meanwhile problems with development of the new software for the Salyut 5B computer lead to the decision to launch Mir with the old analogue Argon computer from Salyut DOS-17K. The digital computer would have to be installed later in orbit.

By April 1985 it was clear that the planned processing flow could not be followed and still make the spring 1986 launch date. The decision was taken on Cosmonautics Day (April 12) to ship the flight model to Baikonur and conduct the systems testing and integration there. Mir arrived at the launch site on 6 May 1985. 1100 of 2500 cables required rework based on results of testing of the ground test model at Khrunichev. In October 1985 Mir was rolled outside of its clean room to conduct communications tests of the Altair system with the Cosmos 1700 satellite already in orbit.

The first launch attempt on 16 February 1986 at very low temperatures was scrubbed when the spacecraft communications failed. The second attempt on 20 February was successful. The political deadline had been met.

The early launch of Mir left the planners without Soyuz spacecraft or modules to launch to it. The decision was taken to launch Soyuz T-15 on a unique dual station mission. The Soyuz would first dock with Salyut 7, which was dead in space, and completely repair the station. They then would fly in their Soyuz to Mir, and put it into initial operation. This spectacular mission marked a new maturity in the Soviet space program.

Just as Mir assembly began in earnest, the Soviet Union disintegrated. The military Spektr module was cancelled and no funds were available for completion of the Priroda earth resources module. Vice President Al Gore and Prime Minister Victor Chernomyrdin signed an agreement for a two-phase International Space Station program at the US-Russian summit in Washington in September 1993. Phase One (1994-96) would involve Shuttle missions to Russia's current Mir station. NASA would pay Russia $100 million annually to keep a 'guest astronaut' on the Mir complex. The money also made it possible for Russia to launch the 'Spektr' and 'Priroda' expansion modules to Mir, with some US experiments onboard. The program was later extended by two more flights in 1998 to help pay for Russia's ISS contributions. In the end, NASA paid the Russians $472 million for nine Shuttle dockings.

Following the end of the US flights, Mir barely continued in operation into the next century. When it became impossible to keep it going by selling visits to foreign customers, it was decided to bring it down in the Pacific Ocean using a specially modified Progress tug. By then it had been in orbit for 15 years. It had been continuously added to, survived crashes with errant spacecraft and space debris, and provided astronauts from many nations with experience in extended space flight. Mir at tis demise consisted of 7 modules with 11.5 tonnes of scientific equipment. It cost $220 to $240 million per year to keep in operation.


Major Events:

  • 1978 August - Mir draft project completed.  Spacecraft: Mir.

    By this time Mir had evolved to the final configuration of one aft port and five ports in a spherical compartment at the forward end of the station. It was planned that the ports would provide docking positions for 7 tonne modules derived from the Soyuz spacecraft. These would use the Soyuz propulsion module, as in Soyuz and Progress, but would be equipped with long laboratory modules in place of the descent module and orbital module.

  • 1982 - During the year - Mir drawing release.  Spacecraft: Mir.

    Drawings for the Mir space station are released during the course of 1982 and 1983 and construction of the spacecraft and its systems are begun.

  • 1984 Spring - Glushko ordered to launch Mir by March 1986.  Spacecraft: Mir.

    By early 1984 work on Mir ground to a halt as all resources were put on getting the Buran space shuttle into flight test. This changed in the spring 1984 when Glushko was called into the office of the Central Committee's Secretary for Space and Defence and ordered to orbit Mir by the 27th Communist Party Congress in the spring of 1986.

  • 1985 May 6 - Mir space station delivered to Baikonur.  Spacecraft: Mir.

    1100 of 2500 cables required rework based on results of testing of the ground test model at Khrunichev.

  • 1985 October - Mir free-air communications tests..  Spacecraft: Mir.

    Mir was rolled outside of its clean room to conduct communications tests of the Altair system with the Cosmos 1700 satellite already in orbit.

  • 1986 February 16 - First attempt to launch Mir..  Spacecraft: Mir.

    The first launch attempt at very low temperatures was scrubbed when the spacecraft communications failed.

  • 1986 February 19 - Mir.  Spacecraft: Mir . Mass: 20,100 kg (44,300 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    The core module of Russia's new space station was placed in an initial orbit of 172 x 301 km. It was established in its operational orbit on 6 March. It passed just 10 km from Salyut 7 on 8 March. First use of the geosynchronous Luch relay sattelite for communications with the station was on 29 March. Equipment launched with the core module included:

    • Splav-2 crystal growth facility
    • Zona zone melt facility
    • Kashtan electrophoresis unit
    • Bulgarian Rozhen photometer
    • Spektr-256 and MKS-M spectrometers
    • Pion-M multipurpose physics unit (41 kg)
    • Biryuza semiconductor materials unit
    • -Ruchei electrophoresis installation
    • Yantar metal coating equipment
    • Mariye magnetic spectrometer
    • Korund furnace (136 kg)

    Total costs of Mir from February 1986 through return of Soyuz TM-9 in April 1989 were given as 1.471 billion rubles. This sum ncluded Mir, Kvant, all Soyuz and Progress spacecraft, and 2 new modules. As of April 1989 50% of the scientific equipment was inoperable and the interior was cramped due to lack of extension modules. Electric power supply problems were first reported in April 1989 (batteries would not hold charge from panels). Mass 27,300 kg as of January 1990. Complex mass with Kvant-2 65,790 kg; with Kristall, Soyuz TM, and Progress M, 89,990 kg.

    Maneuver Summary:
    172 km X 294 km orbit to 170 km X 335 km orbit. Delta V: 11...more.

  • 1986 March 13 - Soyuz T-15.  Spacecraft: Soyuz T. Mass: 7,020 kg (15,470 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Main Expedition EO-01. Epic repair mission. The crew, consisting of ship's commander L D Kizim and flight engineer V A Solovyov first docked with the Mir orbital station to conduct scientific and technical studies and experiments. Mir then maneuvered 17 April to match Salyut 7's orbit at 4000 km separation, then again on 4 May to catch up. After six weeks aboard Mir, Soyuz T-15 undocked on 5 May, then rendezvoused and manually docked with the inoperative Salyut 7 station. This was the only flight in history by a single spacecraft between two space stations. The Salyut-7 station was found to be ice bound and without electrical power. The crew repaired the station, regaining power, heat, and environmental control. The also removed experimental results left behind by last crew. Soyuz T-15 undocked Salyut 7 on 25 June, and redocked with Mir on 26 June, delivering 400 kg of scientific material from Salyut 7, including a multichannel spectrometer. Following further work aboard Mir, the crew landed on July 16, 1986 at 12:34 GMT. No crew ever revisited Salyut 7; it made an uncontrolled reentry over Argentina.

  • 1986 March 19 - Progress 25.  Spacecraft: Progress. Mass: 7,270 kg (16,020 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel transporting sundry cargoes to the Mir orbital station. Docked with Mir on 21 Mar 1986 11:16:02 GMT. Undocked on 20 Apr 1986 19:24:08 GMT. Destroyed in reentry on 21 Apr 1986 00:48:30 GMT. Total free-flight time 2.27 days. Total docked time 30.34 days.

  • 1986 April 23 - Progress 26.  Spacecraft: Progress. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel to Mir. Rendezvoused with Mir on 25 April, but problem with Mir's radio communication system delays docking until the next day. Docked with Mir on 26 Apr 1986 21:26:06 GMT. Undocked on 22 Jun 1986 18:25:00 GMT. Destroyed in reentry on 23 Jun 1986 15:41:01 GMT. Total free-flight time 3.96 days. Total docked time 56.87 days.

  • 1986 May 21 - Soyuz TM-1.  Spacecraft: Soyuz TM. Mass: 7,070 kg (15,580 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Test of new Soyuz vehicle. Recovered May 30, 1986 6:49 GMT. Unmanned test of Soyuz TM. Docked with Mir May 23 1987. Undocked 29 May.
    Officially: Comprehensive experimental testing of spacecraft in independent flight and jointly with the Mir orbital station.

  • 1986 May 28 - EVA Mir EO-1-1.  Spacecraft: Mir.

    Installed truss.

  • 1986 May 31 - EVA Mir EO-1-2.  Spacecraft: Mir.

    Tested truss structure.

  • 1986 July 16 - Landing of Soyuz T-15. 

    Soyuz T-15 landed at 12:34 GMT, 55 km NE of Arkalyk.

  • 1987 January 16 - Progress 27.  Spacecraft: Progress. Mass: 7,230 kg (15,930 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel to Mir; raised Mir's orbit. Transported sundry cargoes to the Mir orbital station. Docked with Salyut 7 on 18 Jan 1987 07:26:50 GMT. Undocked on 23 Feb 1987 11:29:01 GMT. Destroyed in reentry on 25 Feb 1987 16:05:00 GMT. Total free-flight time 4.25 days. Total docked time 36.17 days.

  • 1987 February 5 - Soyuz TM-2.  Spacecraft: Soyuz TM. Mass: 7,100 kg (15,600 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-02. Docked with Mir 7 February 1987. Carried Yuri Romanenko, Aleksander Laveykin to Mir; returned Laveykin, crew of Soyuz TM-3 to Earth.

  • 1987 March 3 - Progress 28.  Spacecraft: Progress. Mass: 7,246 kg (15,974 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel to Mir. Orbit of station at time of rendezvous was 344 X 369 km, 51. 62 deg. Docked with Mir on 5 Mar 1987 12:42:36 GMT. Undocked on 26 Mar 1987 05:06:48 GMT. Destroyed in reentry on 28 Mar 1987 03:49:00 GMT. Total free-flight time 4.01 days. Total docked time 20.68 days.

  • 1987 March 31 - Kvant 1.  Spacecraft: Kvant. Mass: 20,000 kg (44,000 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    MIR module; high energy observatory. Docked with Mir. Rendezvous with Mir 5 April; soft dock 9 April; EVA on 11 April to remove fabric strip from docking apparatus and hard dock; jettisoned service module on 12 April at 22:18

    Maneuver Summary:
    168 km X 278 km orbit to 172 km X 300 km orbit. Delta V: 7 m/s
    169 km X 296 km orbit to 172 km X 314 km orbit. Delta V: 5 m/s
    170 km X 313 km orbit to 297 km X 345 km orbit. Delta V: 46 m/s
    298 km X 344 km orbit to 345 km X 364 km orbit. Delta V: 18 m/s
    Service Module only, after undocking with Mir:
    345 km X 364 km orbit to 341 km X 363 km orbit. Delta V: 1 m/s
    340 km X 361 km orbit to 383 km X 406 km orbit. Delta V: 24 m/s
    Total Delta V: 101 m/s
    Officially: Extra-atmospheric astronomic research and resolution of a number of problems with scientific and economic applications.

  • 1987 April 11 - EVA Mir EO-2-1.  Spacecraft: Mir.

    Removed bag from docking unit that interfered with Kvant docking.

  • 1987 April 21 - Progress 29.  Spacecraft: Progress. Mass: 7,100 kg (15,600 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel to Mir. Deorbited May 11, 1987. Docked with Mir at 343 X 363 1705 23 April at rear port of Kvant. Undocked May 11 03:10. Deorbited28 May 02:59 .
    Officially: Transporting sundry cargoes to the Mir orbital station. Docked with Salyut 7 on 23 Apr 1987 17:04:51 GMT. Undocked on 11 May 1987 03:10:01 GMT. Destroyed in reentry on 11 May 1987 08:28:00 GMT. Total free-flight time 2.30 days. Total docked time 17.42 days.

  • 1987 May 19 - Progress 30.  Spacecraft: Progress. Mass: 7,249 kg (15,981 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vessel to Mir. Rendezvoused with Mir/Kvant in its orbit of 343 X 366 km, 51. 6 deg. Docked with the station on 21 May 1987 05:50:38 GMT. Undocked on 19 Jul 1987 00:19:51 GMT. Destroyed in reentry on 19 Jul 1987 05:42:00 GMT. Total free-flight time 2.30 days. Total docked time 58.77 days.

  • 1987 June 12 - EVA Mir EO-2-2.  Spacecraft: Mir.

    Began solar array installation.

  • 1987 June 16 - EVA Mir EO-2-3.  Spacecraft: Mir.

    Continued solar array installation.

  • 1987 July 22 - Soyuz TM-3.  Spacecraft: Soyuz TM. Mass: 7,100 kg (15,600 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned three crew. Transported to the Mir orbital space station a Soviet-Syrian crew comprising cosmonauts A S Viktorenko, A P Aleksandrov and M A Faris to conduct joint research and experiments with cosmonauts Y Romanenko and A Laveykin. Maneuvered from initial 231 X 217 km orbit to Mir's 311 X 359 km orbit. Docked with rear Mir port at 3:30 GMT 24 July. Undocked with rear port 30 July and docked to forward port.

  • 1987 July 30 - Landing of Soyuz TM-2. 

    Undocked from Mir at 8:34 GMT on 29 July. The Orbital Module was jettisoned before retrofire and left in a 308 X 356 orbit. Soyuz TM-2 landed at 01:05 GMT with the crew of Faris, Laveykin and Viktorenko aboard.

  • 1987 August 3 - Progress 31.  Spacecraft: Progress. Mass: 7,212 kg (15,899 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Rendezvous transfer orbits 187 X 250 km, 51. 64 deg; 266 X 314 km; 309 X 360 km. Docked with Mir on 5 Aug 1987 22:27:35 GMT. Refueled Mir propellants tanks on 15/16 Sept. Undocked on 21 Sep 1987 23:57:41 GMT. Destroyed in reentry on 23 Sep 1987 01:02:00 GMT. Total free-flight time 3.12 days. Total docked time 47.06 days.

  • 1987 September 23 - Progress 32.  Spacecraft: Progress. Mass: 7,035 kg (15,509 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Delivered 850 kg propellants, 315 kg food, 2,000 kg total. Docked with Mir on 26 Sep 1987 01:08:15 GMT. Undocked on 10 Nov 1987 04:09:10 GMT. Redocked from 2,500 m on 10 Nov 1987 05:47 GMT. Undocked again 17 Nov 1998 19:25 GMT. Destroyed in reentry on 19 Nov 1987 00:58:00 GMT. Total free-flight time 3.17 days. Total docked time 52.82 days.

  • 1987 November 20 - Progress 33.  Spacecraft: Progress. Mass: 6,895 kg (15,200 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Space station orbit at rendezvous was 326 km x 343 km. Docked on 23 Nov 1987 01:39:13 GMT. Undocked on 19 Dec 1987 08:15:46 GMT. Destroyed in reentry on 19 Dec 1987 13:37:00 GMT. Total free-flight time 2.30 days. Total docked time 26.28 days.

  • 1987 December 21 - Soyuz TM-4.  Spacecraft: Soyuz TM. Mass: 7,070 kg (15,580 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-03. Carried Musa Manarov, Anatoly Levchenko, Vladimir Titov to Mir; returned crew of Soyuz TM-5 to Earth. Orbits 168 x 243 km, 255 x 296 km, 333 x 359 km. Docked with Mir 12:51 GMT 23 December. 30 December moved to forward port.

  • 1987 December 29 - Landing of Soyuz TM-3. 

    Soyuz TM-3 undocked from Mir at 05:55 GMT and landed near Arkalyk at 09:16 GMT with the crew of Aleksandrov, Levchenko (Soyuz TM-4) and Romanenko (Soyuz TM-2) aboard.

  • 1988 January 20 - Progress 34.  Spacecraft: Progress. Mass: 7,078 kg (15,604 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked on 23 Jan 1988 00:09:09 GMT. Undocked on 4 Mar 1988 03:40:09 GMT. Destroyed in reentry on 4 Mar 1988 07:29:30 GMT. Total free-flight time 2.21 days. Total docked time 41.15 days.

  • 1988 February 26 - EVA Mir EO-3-1.  Spacecraft: Mir.

    Completed solar array installation. Inspected exterior of station.

  • 1988 March 23 - Progress 35.  Spacecraft: Progress. Mass: 7,037 kg (15,513 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked on 25 Mar 1988 22:21:35 GMT. Undocked on 5 May 1988 01:36:03 GMT. Destroyed in reentry on 5 May 1988 06:56:19 GMT. Total free-flight time 2.28 days. Total docked time 40.14 days.

  • 1988 May 10 - Mir News 032: Oncoming operations. 

    During the last weeks of April 1988 it was obvious that there had been some changes in the time schedule for the important operations planned for the end of May and during the month June. On 22 April using the engines of the Progress-35 (then still attached to the Kvant module) the whole complex shifted to a little bit higher orbit. Thus they changed the schedule for meetings (rendezvous ) in the near future, i.e. the Progress-35 and the Soyuz-TM5.

    Previously the meeting with Progress-36 had been planned for approx. 23 May and the arrival of the Soviet-Bulgarian mission by Soyuz-TM5 would originally occur towards the end of June. The preparations for the undocking and destruction of Progress-35 took place according to the original plans. During the last days of April the transfer of the last fuel from that s/c to the base block and the stowing away in Progress-35 of all which they wished to throw away or had to get rid of badly.

    The report of the conclusion of those activities came from Manarov on May 4th during orbit 12693 from 1015-26 UTC. He reported the closing of the hatches and the unlocking of the safety locks against spontaneous undocking. So from this moment on ground control was free to undock the s/c and to put it on the destruction trajectory into the atmosphere. This had been done on May 5th and the Progress-36 burnt away over a silent part of one of the Oceans far outside our window.

    Meanwhile other sources revealed that Progress-36 was on Baykonur ready for launch within a few days. As always the normal question: When? The launch-window for a successful flight to Mir is a small one. I did not need to try to find the answer with difficult calculations as the answer came from Manarov himself. In a conversation with TsUP on 8 May, during orbit 12757 from 1152-1202 UTC, the exact date was of the planned docking of Progress-36 with Mir was mentioned.

    Manarov got orders for certain activities on 14 May and he made objections as this would be "docking day" and after the docking they possibly will be sleeping. Using the updated program for Mir predictions I found that the pass in which the docking operation will be in its final stage will be one with for us a negative elevation: orb. 12848, 0137-0141 UTC with highest elevation -1 degree. I suppose the docking will take place appr. 0149 UTC.

    So the only possibility to be sure about the conclusion of the docking operation will be monitoring the next pass, during orbit 12846, from 0308-18 UTC, which I certainly will do. After the docking of Progress-36 to the docking port of Kvant they will have to do something to get that port free for the arrival of Soyuz-TM5 on June the 9th. They can try to finish operations (unloading, loading and destruction) with Progress-36 as soon as possible or put it to one of the side ports in the transition section, as the axial port of this section is still occupied by Soyuz-TM4. We will wait and hear!

    So June the 7th the launch of the Soyuz-TM5 with captain Anatoliy Solovyov, the mechanic Viktor Savinykh and their Bulgarian guest Aleksandr Aleksandrov. The stand-in crew consists of: captain Vladimir Lyakhov, mechanic Andrey Zaytsev, and the Bulgarian Krasimir Stoyanov. They just started their final training in Baykonur.

    There is more news: a lot of interesting events recently: problems with stinking water on board Mir and extra observations of the sand drifts from the Sahara to the north. They also spoke about the damage to the glass of portholes caused by micro meteorites for instance appr. 1 May 1988. These minuscule damages are being registered by a device with the abbreviation T.I.G.R. This makes it possible to send TV-images , photo's and halograms to the experts on Earth.

    (The abbreviation stands for Television- Interference- Halographic-Registrator ) During a long conversation with -possibly- a scientific journalist in TsUP he gave a lecture about that device during the pass in orbit 12709 on May the 5th.

    Greetings, and for radio amateurs, 73-s, Chris van den Berg, NL-9165/A-UK3202

  • 1988 May 13 - Progress 36.  Spacecraft: Progress. Mass: 7,077 kg (15,602 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Rendezvous transfer orbits 185x246 km, 51. 66 deg; 223x334 km; 331x357 km. Docked with Mir on 15 May 1988 02:13:26 GMT. Undocked on 5 Jun 1988 11:11:55 GMT. Destroyed in reentry on 5 Jun 1988 21:18:40 GMT. Total free-flight time 2.49 days. Total docked time 21.37 days.

  • 1988 May 13 - Mir News 033: Progress-36 launched to Mir.. 

    Based on a report by TsUP to Manarov I expected the launch of Progress-36 in the early morning hours of 12 May ( UTC). This launch did not take place, as there happened to be a postponement of 24 hrs. Why they had to postpone the launch is not known yet and whether it has something to do with the problems with Kosmos-1900, I do not know either. But for sure: Progress-36 is on its way as from 13 May approx. 0030 UTC). Tomorrow, 14 May the cosmonauts have a day off and the planned docking will take place on 15 May 1988.I expect that the docking operation will be in its final phase during the window in orbit 12861 0158-0206UT, azimuth from 178 through 144 to 85 degrees, with max. elevation at 0202 UTC. Possibly the docking itself will take place outside our window at approx. 0214 UTC. During the next orbit 12863 from 0331-0341 UTC the final result of the operation can be checked.

    The plans for the launch of Soyuz-TM5 with 2 Russians and 1 Bulgarian are still unchanged: June the 7th 1988.

    Greetings, and radio amateurs: 73-s,

    Chris van den Berg, NL-9165/ A-UK:3202.

  • 1988 May 15 - Mir News 034: Progress-36 docked to Mir at 1213 UTC. 

    The execution of the docking operation 1 day later was very favourably for our geographical position as the "approach pass" now fully fell within our "radio window". If this operation had been performed yesterday monitoring of that essential pass would have been impossible! Now I again enjoyed the well known schedule, so the first pass of the 24 hrs sequence and after Loss of signal 7 or 8 minutes before docking. So now it was worthwhile to sacrifice a few hours sleep.

    During the pass in orbit 12861 the transmitter worked (from 0154-0206 UTC) and now Titov reported the attitude changes and the fuel consumption to TsUP . For instance at 0202 UTC: Omega Ypsylon 2/10 Z 1/100 Fuel consumption 73.4, heading 06 Pitch 05. TsUP asked something about the horizon and Manarov told them 1.1. and 2.5. At 0203 UTC Titov reported that the Ypsylon gradually increased and he supposed that this meant a revolution (turning of Progress-36) TsUP confirmed this it "turned" and "returned" . As during previous dockings the Telemetry transmitter on 166.125mc did not work. After passing the horizon it Lasted another 7 minutes before the docking was completed (in my previous report I estimated this to be approx. 0214 UTC, so a nice result for this humble SWL) Again I missed the enthusiasm of their predecessors. During the flight of Romanenko the passes after dockings were joyful happenings. During the next pass they just had switched on their transmitter but did not say a word. The report about the "locks" (against spontaneous undocking) came in the pass in orbit 12863 from 0506-0516 UTC. The fact that. they received letters, papers and photographs was mentioned in a contact with a control ship from 0817--0826 UTC. During the last passes they had conversations with their relatives (with duplex TV). Gradually the windows will occur during night hours and so we will have to wait for a more active period when the first windows shift to the evening hours. That is necessary as on 7 June we wilt have to monitor launch and flight of Soyuz-TM with 3 men on board!

    Greetings and radio amateurs, 73-s,

    Chris van den Berg/NL-9165/A-UK3202.

  • 1988 June 6 - Mir News 035: Progress-56 undocked on June 5.. 

    PROGRESS-56: This cargo ship was separated from the Mir station and destroyed. It was expected that this would happen before the launch of Soyuz-TM5, estimated for tomorrow. During the last operation there have been, deviations from schedules used before. Normally the period between the undockng of a freighter and the next launch is longer. During the radio conversation with TsUP during the pass in orbit 13202/13203 from 1849-1854 UTC they spoke about the departure of the Progress-36. Titov reported that they had been able to observe it until the attitude change of the station. Now this was difficult and they had to look for a suitable porthole. Manarov explained that they were positioned on one side. A few minutes later they saw the Progress-36. Titov said that it looked like Venus, even somewhat clearer. At 1853 UTC Manarov made a photograph of the freighter. He did this on a request of TsUP and used a computer for aiming the camera. At 195220 UTC he entered the command via the "display" and made the shot at 1853 UTC sharp. It was a pity that the sky was overcast over here during the periods that the 2 objects were passing. This must have been so the next pass just before the start of the Progress-36 engine at 2028 UTC to reduce its speed for decay in the atmosphere. which followed a few minutes later. Undoubtedly Moscow will speak about 6 June as for Moscow time it was already 6 June., for UTC still 5 June. A few days ago -probably with the use of the Progress engine- they changed altitude. (Somewhat higher, but enough to corrupt all prediction programs). A manoeuvre necessary for a good ballistic configuration for the rendezvous soon to follow.

    SOYUZ-TM5: The last preparations are in progress now on Baykonur . If all goes well the take off will be on 7 June 1988 at 1405 UTC (1805Msc Time) The independent flight will last 2 days and my own calculation (so might deviate much or somewhat) tells me that the docking might take place on 9 June at 1538 UTC. While editing this story the commission did not yet appoint the crew which will fly. Yesterday they all were in good health and so probably the Soyuz will be flown by Solovyov, Savinykh and the Bulgarian Aleksandrov: if not so Lyakhov, Zaytsev and the Bulgarian will have to postpone terrestrial activities for 10 days. During the flight of Soyuz-TM5 there will be radio traffic on 121.750 Mc, (FM) so several ground services on West European airfields can expect funny sounds during there wok. During a previous occasion. Titov reacted on radio traffic of the Airport Rotterdam. (Until now they do not believe that!) After docking with Mir (Kvant port )the main channel for radio traffic will be 143.625 mc again. In Bulgaria there is a lot of enthusiasm and the Observatory of Stara Zagora will act as a sub control station.

    Greetings and radio amateurs 73-s,

    Chris van den Berg, NL-9165/A-UK3202.

  • 1988 June 7 - Soyuz TM-5.  Spacecraft: Soyuz TM. Mass: 7,000 kg (15,400 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Transported to the Mir orbital station a Soviet/Bulgarian crew comprising cosmonauts A Y Solovyev, V P Savinykh and A P Aleksandrov (Bulgaria) to conduct joint research and experiments with cosmonauts V G Titov and M K Manarov. Interim orbit 343 x 282 km. Maneuvered to Mir's 355 x 349 km orbit. Docked 15:57 GMT 9 June to Mir's aft port. Moved to forward port 18 June.

  • 1988 June 17 - Landing of Soyuz TM-4. 

    Undocked 06:18 GMT 17 June 88. Soyuz TM-4 landed at 10:13 GMT, 202 km from Dzehezkazgan, with the crew of Aleksandrov Aleksandr, Savinykh and Solovyov aboard.

  • 1988 June 30 - EVA Mir EO-3-2.  Spacecraft: Mir.

    Began repair of TTM telescope.

  • 1988 July 18 - Progress 37.  Spacecraft: Progress. Mass: 7,065 kg (15,575 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Rendezvous transfer orbits 187x256 km, 51. 62 deg; 235 x 319 km; 343 x 347 km. Docked with Mir on 20 Jul 1988 22:33:40 GMT. Refuelling operations on 7,8, and 9 August 1998. Undocked on 12 Aug 1988 08:31:54 GMT. Destroyed in reentry on 12 Aug 1988 13:45:40 GMT. Total free-flight time 2.27 days. Total docked time 22.42 days.

  • 1988 August 29 - Soyuz TM-6.  Spacecraft: Soyuz TM. Mass: 7,070 kg (15,580 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Transported to the Mir orbital station a Soviet-Afghan crew comprising the cosmonauts V A Lyakhov, V V Polyakov and A A Momand (Afghanistan) to conduct joint research and experiments with the cosmonauts V G Titov and M K Manarov. Returned Manarov, Titov (Soyuz TM-4), Chretien (Soyuz TM-7) to Earth. Initial orbit 195 X 228 km at 51. 57 deg. Maneuvered to a 235 x 259 km orbit, then docked with Mir at 05:41 GMT on 31 August at its 339 x 366 km orbit. Moved from aft to forward port 8 Sept 88.

  • 1988 September 7 - Landing of Soyuz TM-5. 

    Undocked 22:55 GMT 5 September. Jettisoned Orbital Module 23:35 GMT 5 September. Planned landing 02:15 September 6 1988 failed due to confusion of infrared horizon sensors. Repeat retrofire attempt one orbit later resulted in a partial burn only. The crew had to spend a tense 24 hours in the cramped Descent Module (the Orbital Module having already been jettisoned before the retrofire burn) before making last chance deorbit. Finally Lyakhov and Afghani cosmonaut Mohmand (Soyuz TM-6) returned safely to Earth and landed September 7, 1988 00:50 GMT, 160 km SE Dzhezkazgan.

  • 1988 September 9 - Progress 38.  Spacecraft: Progress. Mass: 7,027 kg (15,491 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. During launch first test of Buran ejection seat was made during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Rendezvous orbits 186 X 246 km, 51. 63 deg; 234 X 332 km, 337 X 363 km. Docked with Mir on 12 Sep 1988 01:22:28 GMT. Delivered 2,000 kg supplies including 300 kg of food. Refuelled Mir. Undocked on 23 Nov 1988 12:12:46 GMT. Destroyed in reentry on 23 Nov 1988 19:06:58 GMT. Total free-flight time 2.36 days. Total docked time 72.45 days.

  • 1988 October 20 - EVA Mir EO-3-3.  Spacecraft: Mir.

    Completed repair of TTM telescope. Tested new spacesuit.

  • 1988 November 26 - Soyuz TM-7.  Spacecraft: Soyuz TM. Mass: 7,000 kg (15,400 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-04. Carried Alexander Volkov, Sergei Krikalev, Jean-Loup Chretien to Mir; returned Volkov, Krikalev to Earth. Initial Orbit: 194 X 235 km. Thereafter maneuvered to rendezvous orbit 256 X 291 km before docking with Mir in 337 X 369 km at 17:16 GMT 28 November.

  • 1988 December 9 - EVA Mir EO-4-1.  Spacecraft: Mir.

    Deployed ERA (French experiment).

  • 1988 December 21 - Landing of Soyuz TM-6. 

    Soyuz TM-6 landed at 09:57 GMT with the crew of Chretien, Manarov and Titov Vladimir aboard. Undocked from Mir 21 December 1989 at 03:33 GMTwith the crew of Chretien, Manarov and Titov Vladimir aboard. Revised software installed as a result of TM-5 abort overloaded computer. Landing planned for 06:48 aborted. Backup program used. Orbital Module retained through retrofire. Landed December 21, 1988 09:57 GMT, 180 km SE of Dzhezkazgan.

  • 1988 December 25 - Progress 39.  Spacecraft: Progress. Mass: 7,015 kg (15,465 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Made second test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Rendezvous orbits 187 X 237 km, 51.63 deg; 236 X 338 km; 325 X 353 km at Mir. Delivered 1,300 kg cargo. Docked with Mir on 27 Dec 1988 05:35:10 GMT. Undocked on 7 Feb 1989 06:45:34 GMT. Destroyed in reentry on 7 Feb 1989 13:49:00 GMT. Total free-flight time 2.35 days. Total docked time 42.05 days.

  • 1989 February 10 - Progress 40.  Spacecraft: Progress. Mass: 7,022 kg (15,480 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Conducted third test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Docked with Mir on 12 Feb 1989 10:29:38 GMT. Undocked on 3 Mar 1989 01:45:52 GMT. Unfurled experimental space mirror petal structure on undocking. Destroyed in reentry on 5 Mar 1989 01:59:00 GMT. Total free-flight time 4.08 days. Total docked time 18.64 days.

  • 1989 March 16 - Progress 41.  Spacecraft: Progress. Mass: 6,995 kg (15,421 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Conducted fourth test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Delivered Bulgarian Spektr 256 spectrometer, power supplies for failed equipment. Docked with Mir on 18 Mar 1989 20:50:46 GMT. Between April 9 and 17 boosted Mir into a 373 X 416 km storage orbit after the decision was made to delay remanning the station. However these maneuvers resulted in the spacecraft running out of fuel. Undocked on 21 Apr 1989 01:46:15 GMT. Destroyed in uncontrolled decay of orbit on 25 Apr 1989 12:12:00 GMT. Total free-flight time 6.52 days. Total docked time 33.21 days.

  • 1989 April - Soyuz TM-8A (cancelled).  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb).

    Planned flight to ensure continuous occupation cancelled due to budget cutbacks and delay in launching Kvant 2 and Kristall modules.

  • 1989 April 27 - Landing of Soyuz TM-7. 

    Soyuz TM-7 landed at 02:59 GMT with the crew of Krikalyov, Polyakov and Volkov Aleksandr aboard.

  • 1989 August 23 - Progress M-1.  Spacecraft: Progress M. Mass: 7,270 kg (16,020 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned supply vehicle to Mir; first flight of new vehicle design. Tested on-board systems under different conditions and delivered expendable materials and sundry cargo to the Mir manned space station. Docked with Mir on 25 Aug 1989 05:19:02 GMT. Undocked on 1 Dec 1989 09:02:23 GMT. Destroyed in reentry on 1 Dec 1989 11:21:00 GMT. Total free-flight time 2.19 days. Total docked time 98.16 days.

  • 1989 September 5 - Soyuz TM-8.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned two crew. Mir Expedition EO-05. Docked with Mir 8 September. Transported to the Mir orbital station a team consisting of A S Viktorenko, commander of the spacecraft, and A A Serebrov, on-board engineer, to carry out scientific and technological research and experiments. Flight cost 80 million rubles. Expected return 25 million rubles net profit.

  • 1989 November 26 - Kvant 2.  Spacecraft: Kvant-2. Mass: 19,565 kg (43,133 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    Mir expansion module. Scheduled docking 2 December delayed due to failure of solar panel to extend and failure of automatic rendezvous system. Faults corrected by ground control and docked with Mir December 6, 1989 at 12:21 GMT. Transferred to lateral port December 8.
    Officially: Delivery to the Mir orbital station of additional equipment and apparatus for the purpose of expanding the research and experiments conducted in the interests of science and the national economy.

  • 1989 December 20 - Progress M-2.  Spacecraft: Progress M. Mass: 7,300 kg (16,000 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir; carried US microgravity payload. Delivered various cargoes to the Mir orbital station, including scientific apparatus produced in the United States of America and intended, pursuant to a commercial agreement, for the conduct of experiments on space biotechnology. Docked with Mir on 22 Dec 1989 05:41:21 GMT. Undocked on 9 Feb 1990 02:33:07 GMT. Destroyed in reentry on 9 Feb 1990 07:56:00 GMT. Total free-flight time 2.31 days. Total docked time 48.87 days.

  • 1990 January 8 - EVA Mir EO-5-1.  Spacecraft: Mir.

    Installed star tracker.

  • 1990 January 11 - EVA Mir EO-5-2.  Spacecraft: Mir.

    Retrieved and installed material samples

  • 1990 January 26 - EVA Mir EO-5-3.  Spacecraft: Mir.

    Tested spacesuit. Examined exterior of Kvant 2.

  • 1990 February 1 - EVA Mir EO-5-4.  Spacecraft: Mir.

    Serebrov tested SPK manoeuvring unit.

  • 1990 February 5 - EVA Mir EO-5-5.  Spacecraft: Mir.

    Viktorenko tested SPK manoeuvring unit.

  • 1990 February 11 - Soyuz TM-9.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned two crew. Mir Expedition EO-06. Docked with Mir. Transported to the Mir orbital station a crew comprising the cosmonauts A Y Solovyov and A N Balandin to conduct an extensive programme of geophysical and astrophysical research, experiments on biology and biotechnology and work on space materials science.

  • 1990 February 19 - Landing of Soyuz TM-8. 

    Soyuz TM-8 landed at 04:36 GMT.

  • 1990 February 28 - Progress M-3.  Spacecraft: Progress M. Mass: 7,249 kg (15,981 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 3 Mar 1990 01:04:32 GMT. Undocked on 27 Apr 1990 20:24:43 GMT. Destroyed in reentry on 28 Apr 1990 00:52:00 GMT. Total free-flight time 2.26 days. Total docked time 55.81 days.

  • 1990 May 5 - Progress 42.  Spacecraft: Progress. Mass: 7,011 kg (15,456 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir; last of original design Progress spacecraft. Conducted fifth and final test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Docked with Mir on 7 May 1990 22:45:03 GMT. Undocked on 27 May 1990 07:08:58 GMT. Destroyed in reentry on 27 May 1990 12:27:30 GMT. Total free-flight time 2.31 days. Total docked time 19.35 days.

  • 1990 May 31 - Kristall.  Spacecraft: Kristall. Mass: 19,640 kg (43,290 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    Mir module; materials processing laboratory. Docked with Mir. Kristall: Mass: 19,500 kg. Mass on docking 17,200 kg. Length: 11. 9 m or 13. 73 m?. Solar array span 36 m. Diameter: 4. 35 m. Payload: 7,000 kg. Two compartments. Instrument-Payload Compartment contains food containers, and industrial processing units Krater 3, Optizon 1, Zona 02, and Zona 03. 0. 8 m hatch leads to Junction-Docking compartment. This contains spherical universal docker with two APAS-89 androgynous docking units. These will be used to dock with Buran shuttle and 1,000 kg X-ray telescope to be delivered by Buran in 1991. Third opening houses earth observation cameras.
    Launch originally planned for 30 March 1990. Delayed to April 18, then further delayed due to computer chip problems.
    Launched 31 May 1990 12:33 GMT. Docking scheduled June 6 at 12:36 but delayed due to problem with one of Kristall's orientation engines. Docking successful 10 June at 12:47. On June 11 moved to side port. Work within module began 15 June.
    Spektr: Late 1991 launch. Remote sensing work. Occupies port opposite Kvant 2. Before this occurs Kristall solar arrays will be relocated to Kvant.
    Officially: Specialized module. Experimental-industrial production of semi-conducting materials; refinement of biologically active substances for the production of new medicinal preparations. Cultivation of crystals of different albumine compositions and hybridizatio n of cells. Conduct of astrophysical and technical experiments.

  • 1990 July 17 - EVA Mir EO-6-1.  Spacecraft: Mir.

    Repaired Soyuz TM-9 insulation rip.

  • 1990 July 26 - EVA Mir EO-6-2.  Spacecraft: Mir.

    Dismantled equipment. Temporarily closed damaged hatch.

  • 1990 August 1 - Soyuz TM-10.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned two crew. Docked with Mir. Mir Expedition EO-07. Transported to the Mir manned orbital station the crew consisting of the cosmonauts G M Manakov and G M Strekalov for the purpose of carrying out a programme of geophysical and astrophysical research, biological and biotechnological experiments, and work on space-materials science.

  • 1990 August 9 - Landing of Soyuz TM-9. 

    Soyuz TM-9 landed at 07:35 GMT, 70 km from Arkalyk at 50 deg 51'E 67 deg 17' N.

  • 1990 August 15 - Progress M-4.  Spacecraft: Progress M. Mass: 7,294 kg (16,080 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Delivered cables for rewiring operations and equipment for Soyuz TM-11 Japanese journalist flight. Docked with Mir on 17 Aug 1990 05:26:13 GMT. Undocked on 17 Sep 1990 12:42:43 GMT. Destroyed in reentry on 20 Sep 1990 11:42:49 GMT. Total free-flight time 5.02 days. Total docked time 31.30 days.

  • 1990 September 27 - Progress M-5.  Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Included first Progress recoverable capsule for return of 150 kg of payload to earth. Docked with Mir on 29 Sep 1990 12:26:50 GMT. Undocked on 28 Nov 1990 06:15:46 GMT. After deorbit burn, capsule separated for reentry with an expected landing in Kazakhstan at 28 Nov 1990 11:04:05 GMT. However the recoverable capsule's beacon signal was never received after reentry. All experimental data and materials in capsule lost. Total free-flight time 2.28 days. Total docked time 59.74 days.

  • 1990 October 30 - EVA Mir EO-7-1.  Spacecraft: Mir.

    Attempt to repair Kvant 2 hatch.

  • 1990 December 2 - Soyuz TM-11.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Docked with Mir. Mir Expedition EO-08. Transported to the Mir manned orbital station the international crew consisting of the cosmonauts V M Afanasyev, M Kh Manarov, and T Akiyami (Japan) for the purpose of carrying out joint work with the cosmonauts G M Manakov and G M Strekalov. Launched jointly with the private Japanese company TBS. The Japanese television network ended up paying $ 28 million for the first commercial flight to Mir to put Akiyama, the first journalist in space aboard Soyuz TM-11. Akiyama made daily television broadcasts.

  • 1990 December 10 - Landing of Soyuz TM-10. 

    Soyuz TM-10 landed at 06:07 GMT, 69 km NW Arkalyk, with the crew of Akiyama, Manakov and Strekalov aboard.

  • 1991 January 7 - EVA Mir EO-8-1.  Spacecraft: Mir.

    Completed repair of Kvant 2 hatch.

  • 1991 January 14 - Progress M-6.  Spacecraft: Progress M. Mass: 7,125 kg (15,707 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Delivered new life support equipment to replace life-expired equipment aboard. Docked with Mir on 16 Jan 1991 16:35:25 GMT. Undocked on 15 Mar 1991 12:46:41 GMT. Destroyed in reentry on 15 Mar 1991 18:07:26 GMT. Total free-flight time 2.30 days. Total docked time 57.84 days.

  • 1991 January 23 - EVA Mir EO-8-2.  Spacecraft: Mir.

    Installed Strela boom on Mir.

  • 1991 January 26 - EVA Mir EO-8-3.  Spacecraft: Mir.

    Installed solar array supports.

  • 1991 March 19 - Progress M-7.  Spacecraft: Progress M. Mass: 7,307 kg (16,109 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Attempted to dock with Mir on 21 March 1998 14:28 GMT, but missed the station by 500 m. Docking attempted again on 23 March but at 50 meters the docking was aborted; the Progress missed hitting the station by five meters. Thereafter it was placed in a station-keeping co-orbit with Mir while the problem was diagnosed. Finally docked with Mir on 28 Mar 1991 12:02:28 GMT. On 12 and 14 Apr 1998 two burns of the engine of Progress M-7 raised the station's orbit from a 360 x 377 km orbit to a 370 x 382 km orbit. Undocked on 6 May 1991 22:59:36 GMT. Destroyed in reentry on 7 May 1991 17:20:05 GMT. Total free-flight time 9.72 days. Total docked time 39.46 days.

  • 1991 April 26 - EVA Mir EO-8-4.  Spacecraft: Mir.

    Inspected Kurs docking system antenna.

  • 1991 May 18 - Soyuz TM-12.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Docked with Mir. Mir Expedition EO-09. Carried Anatoli Artsebarski, Sergei Krikalev, Helen Sharman to Mir; returned Artsebarski, crew of Soyuz TM 8 to Earth. Second commercial flight with paying British passenger. Sponsoring British consortium was not quite able to come up with money, however. Flight continued at Soviet expense with very limited UK experiments.

  • 1991 May 26 - Landing of Soyuz TM-11. 

    Soyuz TM-11 landed at 10:03 GMT with the crew of Afanasyev, Manarov and Sharman aboard.

  • 1991 May 30 - Progress M-8.  Spacecraft: Progress M. Mass: 7,296 kg (16,084 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 1 Jun 1991 09:44:37 GMT. Undocked on 15 Aug 1991 22:16:59 GMT. Destroyed in reentry on 16 Aug 1991 06:56:32 GMT. Total free-flight time 2.43 days. Total docked time 75.52 days.

  • 1991 May 30 - Naduvaniy gazovoy ballon.  Launch Site: Baikonur. Launch Vehicle: Soyuz.

  • 1991 June 17 - Mak 1.  Spacecraft: Mak. Launch Site: Baikonur. Launch Vehicle: Proton.

    Deployed from MIR 6/17/91. Launched from Mir airlock. Investigation of features at the Earth's atmosphere. Launched with the Mir orbital station.

  • 1991 June 25 - EVA Mir EO-9-1.  Spacecraft: Mir.

    Replaced Kurs docking system antenna.

  • 1991 June 28 - EVA Mir EO-9-2.  Spacecraft: Mir.

    Attached TREK cosmic ray collector to exterior of station.

  • 1991 July 15 - EVA Mir EO-9-3.  Spacecraft: Mir.

    Began Sofora girder construction. Sofora mounting platform installed.

  • 1991 July 19 - EVA Mir EO-9-4.  Spacecraft: Mir.

    Began assembly of Sofora girder.

  • 1991 July 23 - EVA Mir EO-9-5.  Spacecraft: Mir.

    Continued assembly of Sofora girder.

  • 1991 July 27 - EVA Mir EO-9-6.  Spacecraft: Mir.

    Completed assembly of Sofora girder.

  • 1991 August - Soyuz TM-13A (cancelled).  Spacecraft: Soyuz TM.

    Soyuz TM-13 and TM-14 crews were reshuffled extensively due to commercial considerations and necessity of flying a Kazakh cosmonaut. This was the original crew assignment. Kaleri and Avdeyev were replaced by Kazakh researchers in the final crew.

  • 1991 August 20 - Progress M-9.  Spacecraft: Progress M. Mass: 7,311 kg (16,117 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir; carried reentry capsule for return of 150 kg of experiment results. Docked with Mir on 23 Aug 1991 00:54:17 GMT. Undocked on 30 Sep 1991 01:53:00 GMT. 350 kg return capsule detached from the Propess' orbital module at an altitude of 110 to 130 km. The capsule underwent a ballistic descent to 15 km, followed by a parachute descent from there to surface. The capsule's beacon began transmitting at 4.5 km. Landed in Kazakhstan on 30 Sep 1991 08:16:24 GMT. Total free-flight time 2.35 days. Total docked time 38.04 days.

  • 1991 October 2 - Soyuz TM-13.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned three crew. Docked with Mir. Mir Expedition EO-10. Transported to the Mir manned orbital station an international crew comprising the cosmonauts A Volkov (USSR), T Aubakirov (USSR) and F. Viehbock (Austria), to conduct joint scientific and technical research with the cosmonauts A. Artsebarsky and S Krikalev. Austria paid $ 7 million for mission. Kazakh cosmonaut added at last minute.

  • 1991 October 10 - Landing of Soyuz TM-12. 

    Soyuz TM-12 landed at 04:11 GMT with the crew of Artsebarsky, Aubakirov and Viehboeck aboard.

  • 1991 October 17 - Progress M-10.  Spacecraft: Progress M. Mass: 7,306 kg (16,106 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. First attempted to dock with Mir on 19 October 1991. The docking was automatically aborted at a distance of 150 m from the station. Successfully docked with the forward port of Mir on on 21 Oct 1991 03:40:50 GMT. Unloading began next day. Undocked on 20 Jan 1992 07:13:44 GMT. Destroyed in reentry on 20 Jan 1992 12:03:30 GMT. Total free-flight time 4.35 days. Total docked time 91.15 days.

  • 1991 End - Soyuz TM-14A (cancelled).  Spacecraft: Soyuz TM.

    Soyuz TM-13 and TM-14 crews were reshuffled extensively due to commercial seat bookings by Austria and Germany and the necessity of flying a Kazakh-born cosmonaut as part of the Baikonur rental agreement. This was the original crew assignment. The Kazakh researchers were moved to the earlier Soyuz TM-13 flight.

  • 1991 End - Soyuz TM-14B (cancelled).  Spacecraft: Soyuz TM.

    Soyuz TM-13 and TM-14 crews were reshuffled extensively due to commercial seat bookings by Austria and Germany and the necessity of flying a Kazakh-born cosmonaut as part of the Baikonur rental agreement. This was the second crew assignment. The Kazakh researchers were moved to the earlier Soyuz TM-13 flight and paying German researchers took their place in the final crew.

  • 1991 December - Soyuz Buran Support (cancelled).  Spacecraft: Soyuz TM.

    Planned Soyuz flight to Mir. Main purpose was to provide spaceflight experience to Bachurin and Borodai, who had been selected as back-up crew of the first manned Buran flight. Cancelled in cut-backs after fall of the Soviet Union.

  • 1991 December 5 - Mir News 115: Mir solar panel damaged by space debris.. 

    On 4 Dec. 1991 during pass in orb. 33171 (1103 UTC) Volkov spoke with a Pyotr (might have been Klimuk) about the Ukraine. Volkov made a passing reference to the fact that the crew discovered 2 small holes In one of the solar panels of Module-D. About this damage the cosmonauts spoke during the first 3 passes on 5 Dec. 1991. They made images with a TV camera, but these were not good enough for analyses. To get better images the cosmonauts had to install a special camera in the transition section (P.Kh.O.) and therefor they had to deploy and connect a cable. In Krikalyov's opinion the only way to get a good insight in the damage a space-walk (EVA) will be necessary. On 5 Dec. they spoke about 2 great holes and 1 small hole. Krikalyov even uttered the possibility that the damage has been arisen during the period in which the American Space shuttle 44, Atlantis, had to alter course to avoid a collision with the 3rd of a Soviet rocket launched long ago. So again a substantial problem for the cosmonauts. For a long time the crew are struggling with the water regeneration system Elektron and the attitude control of the complex.

    During the last days Mir almost permanently remained in sunlight and for the orientation of the sensors they used sun-vectors.

    DIVERTING CAPABILITIES OF THE Mir-COMPLEX IN CASE OF 'COLLISION DANGER' :

    In comparison with the American (and Soviet-) Space Shuttles the Mir-station is a 'lame duck '. Even if Norad (or its Soviet opposite side) would warn Mir and TsuP for an object on collision course a quick diverting manoeuvre cannot be executed (within a few minutes). With the engines of the freighter Progress-M and the ferry Soyuz-TM the altitude of the complex can be altered, but this process lasts too long for comfort. The present crew consist of phlegmatic and crisis proof cosmonauts and they seem not to bother about this all. During radio amateur conversations they state that all is going well.

    1ST STAGE ENERGIYA ROCKET BLOWN UP DURING FIRE TEST:

    This news comes from a radiologist in Omsk, N. Spinov. S., also a member of the State Committee for Ecology, reported that on 20 November 1991 near the village Krutaya Gorkia (55 KM from the Siberian town Omsk) the 1st stage of the Energiya rocket exploded due to a failure in the cooling system. In a huge orange cloud the heath of the explosion dispersed and S. demands a detailed investigation for during the last years the number op persons suffering of cancer alarmingly increased.

    (The 1st stage of the Energiya consists of 4 'strap on' boosters, each of which is a modified version of the 1st stage of the Zenith (SL-16) rocket. Fuel is kerosene, oxidiser LOX).

    Chris van den Berg, NL-9165/A-UK3202

  • 1992 January 19 - Mir News 118: MOSCOW TIME. 

    For those monitoring Radio Moscow: last night Moscow time changed. The clocks have been put 1 hour forward and the new time can be considered to be an interim time. It is called: Sunlight Saving Time and will be valid until 29 March 1992. In the night from 28 to 29 March 1992 the clock will move 1 hour forward again. 50 Moscow time is now UTC+3. (TsUP, and the cosmonauts already used UTC+3 and consequently TsUP/Mir-time is now equal to Moscow time.)

    ATTITUDE CONTROL FAILURE HAMPER IMPORTANT OPERATIONS.

    During the last weeks preparations were going on to make the return capsule ready for a safe return to Earth. This capsule on board freighter Progress-M10 on 18 January 1992 had to separate from the then undocked Progress-MIG for a safe descent. On 16 January 1992 the cosmonauts reported failure of the Attitude Control System. On 17 January 1992 experts on TsUP were still considering what to do, but they already postponed the undocking of the Progress-M10. About the planned launch of Progress-M11 on 21 January 1992 they were not sure. Krikalyav suggested TsUP to carry out both operations and he uttered some alternatives for the attitude control. Until and inclusive 18 January 1992 Progress-M10 has not been used for an orbit correction either.

    (PROGRESS-M11: The crew confirmed that Progress-M1l will not be equipped by a return-capsule. So the original plan to use such a capsule with Progress-M11 has been cancelled.

    Chris van den Berg, NL-9165/A-UK3202

  • 1992 January 25 - Progress M-11.  Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 27 Jan 1992 09:30:43 GMT. Undocked on 13 Mar 1992 08:43:40 GMT. Destroyed in reentry on 13 Mar 1992 15:47:00 GMT. Total free-flight time 2.36 days. Total docked time 45.97 days.

  • 1992 February 21 - EVA Mir EO-10-1.  Spacecraft: Mir.

    Dismantled equipment.

  • 1992 February 21 - Mir News 122: Mir EVA. 

    The EVA started on 20 Febr. 1992 at 2010 UTC and lasted until 21 Febr. 1992 at 0022 UTC. During the pass in orb. 34398, 23041 UTC, the EVA was still going on Krikalyov told TsUP that Volkov felt very well. TsUP asked for Volkov's condition for Volkov had problems with the cooling of his space-suit. The autonomous life support system in his backpack had a malfunction. He tried to cool down by hiding in the shadow, but this did not work. So he connected his spacesuit with the life-support connection near the hatch of Module-D, switched of his autonomous system and continued his work. (Press reports said that he had to go back inside the complex, but he stayed outside.) The cosmonauts removed and changed experiments with materials which had been in space for a long time. The effects of outer space on these materials, to be used for the construction of space vehicles. Krikalyov retrieved some solar cells, which had been fixed on a little experimental solar-battery. The effects of outer space on the endurance and capacity of these cells will he studied on earth. During the EVA the cosmonauts had to try to clean some windows, but they had to skip this.

    During the next 3 passes (at 0037. 0213 en 0347 UTC) there was a lot of radio traffic. After his return on board Kkrikalyov was cold for a long time. He also had some skin-irritation of his hands caused by his gloves and moisture. Volkov recommended him to use a green cream. For this crew this has been the last EVA during this expedition.

    RELIEF AND STAND-INN CREWS:

    On February 19th, together with their German guests, these crews started their final training for the flight with Soyuz-TM14 on 17 March 1992. This final training takes place in Starcity.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1992 February 27 - Mir News 123: Russian Space Agency created. 

    YELSTIN SIGNED DECREE FOR THE ESTABLISHMENT OF THE R.K.A.:

    R.K.A. stands for Rossiyskoe Kosmicheskoye Agentsvo, so Russian Space Agency. For a long time the Russian parliament discussed about the need to establish such an organisation. Its tasks and possibilities, but also the relation to parliament and government, are almost equal to that of the American NASA. Projects for space-operations have to be submitted to that R.K.A. The R.K.A. investigates the project and evaluates the need, necessity, costs and eventual contribution from state-funds. Projects aimed to achieve political- or chauvinistic prestige will not have any chance. After analysing a project this will be send to the parliament for consent about eventual funding. The president can put his veto on it. After consent the project will be send back to R.K.A. R.K.A. asks for offers of firms, scientific institutes, enterprises, national as well as international ones, on the basis of free enterprise and free market and selects those who will get the order(-s). After that R.K.A. has to keep control on the execution of the orders. It will take some time before such an organisation is operational and in fact it is already a little bit late.

    RIDICULOUS AND EXAGGERATED INFORMATION ABOUT BAD HEALTH AND MOOD OF Mir CREW:

    For a long time, more or less caused by 'glasnost' and the bad economic situation in the CIS-states, the (ex-) Soviet press critically and even with denigration reported about their national space exploration. For a few weeks that same press gradually seem to be inclined to change this policy a little bit due to a moderate positive attitude towards 'space' of Yeltsin. A lot of Russian journalists still entertain grievances about the fact, that not a Russian, but a Japanese journalist flew in a Russian space-station. Average reports about space-station Mir are still below zero and a lot these reports find their way to the West. Regretfully the spokesmen and public relations officers of space-organisations in the CIS are still very passive and miss the skill and willingness of their western colleagues to fight for their cause. Negative reports, for instance articles in Komsomolskaye Pravda, Izvestiya and others, are extra exaggerated while proceeding along western press-channels. The cosmonauts hear a lot from western news-agencies and from radio-amateurs around the world and sometimes do not believe their ears. On Febr. 17th Moscow-TV relayed a direct TV-session with Mir and the viewers could see how healthy and active the cosmonauts were. I myself know by day to day observations that the crew has a very good health and a high morale. Of course they meet problems, technical failures, even serious ones, but they always keep good hearth and in co-operation with experts on TsUP they resolve problems by repairing or replacing equipment or systems. Radio-amateurs, who have the possibility to communicate with the crew or to exchange information via Packet Radio, certainly will share my opinion. I will advise you all: take all press-reports about Mir, not with a pinch, but with some pounds of salt.

    C.M. van den Berg, NL-9165/A-UK3202.

  • 1992 March 17 - Soyuz TM-14.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-11. Joint flight with Germany. Docked at the Kvant rear port at 12:33 GMT on March 19.

  • 1992 March 25 - Landing of Soyuz TM-13. 

    Soyuz TM-13 landed at 08:51 GMT with the crew of Flade, Krikalyov and Volkov Aleksandr aboard.

  • 1992 April 19 - Progress M-12.  Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 21 Apr 1992 23:21:59 GMT. Undocked on 27 Jun 1992 21:34:44 GMT. Destroyed in reentry on 28 Jun 1992 00:02:51 GMT. Total free-flight time 2.18 days. Total docked time 66.93 days.

  • 1992 May 30 - Mir News 132: Experiments have priority.. 

    The cosmonauts o.b. Mir have been working on experiments instead of repairing and replacing life-support equipment. They used a camera named Liva for earth-observations and mentioned the areas of which they had to make video recordings. The crew also used equipment for the Austrian experiments of Austromir. They worked on a few of those experiments in co-ordination with an expert on TsUP. Monimir (reflexes under micro-gravity) and Migmas (raster ion microscope) of which the data with the device Datamir are transmitted via Mir's telemetry Monimir (reflexes under micro-gravity) and Migmas (raster ion microscope) of which_the_data_with_the_device_Datamir_are_transmitted_via_Mir's_telemetry channels. The continuation of experiments with equipment left behind by guest cosmonauts must be of a great advantage: funds for Russian spaceflight and the fact that the Austrians have constructed the equipment not only for the short stay on board Mir of Franz Viehbock in Oct. 1991.

    THE EX-TRACKING FLEET: Some of the ships of that fleet are still seaborne, but not for tracking or relay purposes. During the last weeks there have been messages that the Kosmonavt Yuriy Gagarin, the K. G. Dobrovolskiy, the K.V. Komarov and the K.P. Belyayev left their home ports. Obviously the ships made short cruises. It took some investigation work to get the following information: the Russians decided to keep the ships floating and to maintain the original shape as to make the ships 'attractive' for foreigners during cruises and business trips and eventual expeditions. Important persons involved in spaceflight, science and commerce founded some organisations to use the ships for cruises and business promotion trips. They already started one or more cruises. One of the travel agencies is leaded by the former cosmonaut Beregovoy. If they pay 350 thousand rubles cosmonauts and spaceflight employees can enjoy a cruise. A few days ago the Kosmonavt Pavel Belyayev showed up in radio contacts with the Mir station. So just as it has been before: Mir traffic in the West while Mir was still out of range of Yevpatoriya. The Belyayev visited Hamburg with the Mir station. So just as it has been before: Mir traffic in the West while Mir was still out of range of Yevpatoriya. The Belyayev visited Hamburg and the mayor of that city greeted the cosmonauts. Some experts on board kept the transceiver for Mir communications in good order and the scientist and tradesmen on board Belyayev spoke with the cosmonauts. The ship does not work for TsUP and on 30 May, during orbit 35950, 1106-1117 UTC wondered with whom the crew has been speaking. On 1 June the ship will visit London and some important passengers on board will speak with Mir during orbits 35982 (1049-1100 UTC) and 35983 (1225-1235 UTC). Some scientist and tradesmen on board will try to promote Russian products and look for partners for commercial and scientific co-operation. There will be not much propaganda for spaceflight for they do not have much material on board. They have photographs, but no TV-films. Viktorenko told the ship that he regretted this. The Belyayev will be involved in a number of events in relation to the Columbus-92 expeditions and Viktorenko promised that the Mir-crew if necessary and possible will co-operate and assist. There are rumours that an ex-tracking ship (Belyayev or Dobrovolskiy) will visit Rotterdam for 2 days around 10 June 1992.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1992 June 27 - Mir News 134: Progress-M13. 

    Launch of this freighter still on schedule for 30 June 1992. Russian spaceflight authorities now have to take in account interests and feelings of the population, about which they - under protection of the former Soviet Mil. Industrial complex- never bothered. The people living in the Novosibirsk area always feared launches from Baykonur. After launches parts of the rockets (1st stages, hatches, etc.) fall down in that area. Thus far no accidents or damages have been reported -this in contradiction to the ground track areas in Kazakhstan-, but people is always aware of space-launch hazards. To cultivate more goodwill and understanding for space-flight the Baykonur launch-site authorities invited representatives of the administration, civil defence and press of the Novosibirsk region to attend the launch of Progress-M13 on the spot.

    EXTRA VEHICULAR ACTIVITY (SPACEWALK):

    This EVA will take place on 8 or 10 July 1992. The work to be done by the cosmonauts during that EVA is crucial for the operational existence of the Mir complex. 4 of the 6 gyrodynes in Module-D are out of order and so the attitude control of the complex is working unsatisfactorily. For the repair work during the next EVA equipment and tools have to be delivered to Mir by Progress-M13 on 2 July 1992. In the future more work to restore the SUD (movements control system) must be done. For a provisional solution (to keep control on the roll, X- axis, of the complex)f the next crew (Solovyov and Avdeyev) will have to install the VDU (external movements control motor) in the top of the Sofora girder.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1992 June 28 - Mir News 135: Progress-M12. 

    OPERATIONS CONCLUDED.

    To make the docking of the freighter Progress-M13 on 2 July 1992 possible, the Progress-M12 had to disappear. Progress-M12 had been docked to the forward docking port (PKhO) on 22 April and was often used to correct the orbit of the complex. This also happened a few days ago and so only Kepler elements from day 178 or younger are useable. Radio traffic in the night from 27 to 28 June 1992 revealed that the undocking operation was going on. Kaleri watched the undocking and autonomous flight of Progress-M12 from the airlock (S.Sh.O.) of Module-D and Viktorenko observed all what was happening from the base block. During the pass in orb. 36394, which began at 2129 UTC, Progress-M12 separated from Mir. This was right over our heads at 2135 UTC. Telemetry and Doppler beacon (resp. on 166, 165 and 922.755 mc) could be heard. TsUP received TV images made by Kaleri. For a long time Mir and Progress-M12 flew in formation. During the next pass (in orb. 35395, 2306- UTC) Progress-M12 still flew autonomously still more or less observed by Kaleri. At 230654 UTC the exact TCA could be determined (922.755mc passed the BFO-dip). Almost on this moment Progress-M12's rocket worked to reduce its speed and it entered the earth's atmosphere. It decayed (burnt up) at 2321 UTC on 27 June 1992, so 9 minutes after our LOS. Progress-M12 had not been equipped with a return capsule.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1992 June 30 - Progress M-13.  Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. An initial docking attempt on 2 Jul 1992 was a failure. Docked with Mir on 4 Jul 1992 16:55:13 GMT. Undocked on 24 Jul 1992 04:14:00 GMT. Destroyed in reentry on 24 Jul 1992 08:03:35 GMT. Total free-flight time 4.17 days. Total docked time 19.47 days. It was docked to Mir for only a few weeks, since on 26 Jul the Soyuz TM-15 was to be launched with a replacement crew and would need to use the same docking port.

  • 1992 July 4 - Mir News 137: Progress-M13. 

    2D DOCKING ATTEMPT SUCCESSFUL ON 4 JULY 1992 AT 1707 UTC.

    During the first pass here in orb. 36500, 1648-1653 UTC, Progress-M13 was still flying autonomously for she still transmitted on a frequency which has to be quiet during the final approach and after docking. Viktor (Savinykh or Afanasyev) on board of the former tracking ship Belyayev tried to get in touch with Mir, but Kaleri asked him to keep quiet for the docking operation was about to begin. Kaleri told TsUP that they did not see Progress-M13 neither visual nor on their screens. So for abt. 1.5 hour I did not know whether Progress-M13 had been docked or not. During the pass in the next orbit 36501, 1823-1841 UTC, the crew reported that the air-seal was perfect. Progress-M13 had been docked to Mir's forward port at 1707 UTC. Viktorenko told TsUP that they would open the hatch to Progress-M13 as soon as TsUP ordered them to do so. TsUP did this and the cosmonauts crept to the hatch and opened it at 1837 UTC. During the following pass Kaleri reported the good state of the Progress-M13: all was clean. Crew and TsUP exchanged congratulations and the crew thanked the specialists on TsUP for the excellent achievement and TsUP's care for the crew.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1992 July 8 - EVA Mir EO-11-1.  Spacecraft: Mir.

    Inspected gyrodyne orientation flywheels.

  • 1992 July 27 - Soyuz TM-15.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-12. Russian astronauts Solovyov and Avdeev and French astronaut Tognini were inserted into an initial 190 x 200 km orbit inclined 51.6 deg. Later on July 27 they maneuvered to a 223 x 343 km orbit, and on July 28 docked with Mir in its 405 x 410 km orbit.

  • 1992 August 10 - Landing of Soyuz TM-14. 

    The Soyuz TM-14 crew, Aleksandr Viktorenko and Aleksandr Kaleri, returned to Earth together with French astronaut Michel Tognini. The Soyuz TM-14 undocked from Mir at 21:47 GMT on August 9, and landed in Kazakhstan at 01:07 GMT on August 10.

  • 1992 August 15 - Progress M-14.  Spacecraft: Progress M. Mass: 7,176 kg (15,820 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Progress M-38 was specially modified to carry the first VDU (Vynosnaya Dvigatel'naya Ustanovka, External Engine Unit) propulsion unit. The VDU was mounted externally on a special structure between the cargo module and the service module, replacing the OKD fuel section present on normal Progress vehicles. The crew spacewalked to extract the VDU from Progress and place it on the end of the Sofora boom extending from the Kvant module. The VDU was used to provide attitude control capability for the Mir station. Docked with Mir on 18 Aug 1992 00:20:48 GMT. Undocked on 21 Oct 1992 16:46:01 GMT. Destroyed in reentry on 21 Oct 1992 23:12:00 GMT. Total free-flight time 2.35 days. Total docked time 64.68 days.

  • 1992 September 3 - EVA Mir EO-12-1.  Spacecraft: Mir.

    Began installation of VDU thruster pod on Sofora tower.

  • 1992 September 4 - Mir News 145: 1st Solovyov/Avdeyev. 

    This EVA started on 3.09.92 at 1330 UTC (opening hatch airlock Module-D) and ended at 1749 UTC. This EVA is the 1st one in a series to install the VDU (External Movements Control Motor) in the Sofora girder of Kvant-1. The cosmonauts achieved the goals of this EVA. They worked on the container in which the motor was delivered by the freighter Progress-M14. The cosmonauts will continue this work on 7.09.92. It had been expected that during this EVA the cosmonauts would haul down the Soviet flag still waving in the top of the Sofora girder. They only replaced the flag, but certainly will remove it during one of the next 3 or 4 EVA's.

    During the EVA's OM Peter monitored the traffic from the Altair satellite. This traffic will be analysed later.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1992 September 7 - EVA Mir EO-12-2.  Spacecraft: Mir.

    Continued installation of VDU thruster pod on Sofora tower.

  • 1992 September 11 - EVA Mir EO-12-3.  Spacecraft: Mir.

    Completed installation of VDU thruster pod on Sofora tower.

  • 1992 September 15 - EVA Mir EO-12-4.  Spacecraft: Mir.

    Installed Kurs docking system antenna on Kristall module.

  • 1992 September 25 - Mir News 147: Mir-CREW. 

    After the installation of the VDU (Movements Control Motor) in the Sofora girder the cosmonauts got time to work on other matters. They produced semi-conductor materials in the ovens of the Kristall-module and executed a lot of geophysical observations. They made photo's and spectographic images of the earth surface in a number of CIS-republics. These images will help scientists to get more information about the ecological situation of agricultural areas and water basins. With the Krater-5 oven in the Kristall module they on 23.09.92 continued experiments which had been started by the French cosmonaut Tognini. Among these experiments the Superconconduction. This experiments last 130 days. Under high critical temperatures crystallisation of the materials Barium and Copper.

    Movements control of the complex: About the functioning of the VDU (external movements control motor) the cosmonauts did not speak a lot. A spokesman of TsUP declared that this VDU was functioning normally. (This has been denied later on. It was impossible to use the VDU due to software problems.)

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1992 October 1 - Mir News 149: Problems with Mir-TsUP relays work Yevpatoriya.. 

    Disagreements between Russia and the Ukraine about the Black- sea fleet, the Crimea, monetary matters and the former Soviet army on Ukraine's territory for a long time threatened the functioning of the tracking station Yevpatoriya and other radio stations. Half a year ago Yevpatoriya almost had to cease operations due to lack of money. The French government subsidised the station on request of French astronomers who feared that they would lose the input of the satellite Granat, carrying French experiments under control of Yevpatoriya. During recent EVA-s now and then communications between Mir and TsUP were interrupted. As of 21.09.92 no traffic could be heard on 143.625 mc. This traffic came back on 29.09.92. Thus far there has been no telemetry on 166 and 165 mc, so possibly the Russians now use a temporary facility on Russian territory.

    YEVPATORIYA PRIVATISED:

    The Ukrainian government privatised the tracking station Yevpatoriya and forced the staff to be sworn in. Russian has to pay an enormous amount of money for the continuation of Yevpatoriya's services. Russia is not inclined to do so and is trying to find alternatives. As long as the Ukraine does not receive money for the station there is no money to pay the wages of the staff. On 1.10.92 the staff went on strike. Possibly TsUP is now supported by a temporary station on Russian territory for during the passes in orbits nr. 37878, 37879 and 37880 traffic was relayed during the window of Yevpatoriya. There still has been no Telemetry on the normal channels in the 166 and 165 mc bands. Some officials in Kalingrad near Moscow uttered the suggestion to put back in operation one or more tracking ships to fill up the gap caused by the 'radio silence' of Yevpatoriya.

    PROGRESS-M14: This freighter is still attached to the aft (Kvant-1) docking port of the complex. The undocking and decay of Progress-M14 has been planned for 22.10.92. The return capsule will have to make a soft landing while Progress-M14 will burn up.

    PROGRESS-M15: Thus far the launch of this freighter was expected to take place on 5.10.92, but this is impossible due to the delayed departure and decay of its predecessor.

    VDU (EXTERNAL MOVEMENTS CONTROL MOTOR in Sofora girder):

    A spokesman of NPO-Energiya declared that this VDU is perfect in technical respects, but that it has not been used so far. Scientist are computing calculations for the oncoming functioning of the VDU.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1992 October 27 - Progress M-15.  Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 29 Oct 1992 19:05:51 GMT. Undocked on 4 Feb 1993 00:44:53 GMT. After completion of the Znamya and autonomous operation experiments, destroyed in reentry on 7 Feb 1993 06:43:20 GMT. Total free-flight time 5.32 days. Total docked time 97.24 days.

  • 1992 October 27 - Mak 2.  Spacecraft: Mak. Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Deployed from MIR on 11/20/92. Launched from Mir airlock. Conduct of experiments to study physical processes in the Earth's ionosphere. Small satellite launched from the Mir station.

  • 1992 October 27 - Znamya-2.  Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Reflector mirror, deployed from Progress M-15 after separation from Mir space station.

  • 1993 January 24 - Soyuz TM-16.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Manned two crew. Mir Expedition EO-13. Transported to the Mir manned orbital station a crew of the thirteenth main expedition comprising the cosmonauts G M Manakov and A F Poleschuk.The Soyuz carried the APAS androgynous docking system instead of the usual probe system.

  • 1993 February 1 - Landing of Soyuz TM-15. 

    Aleksandr Solovyov and Sergey Avdeyev undocked from the Mir complex aboard Soyuz TM-15 on February 1 and landed the same day in Kazakhstan after six months in space at 03:47 GMT. Soyuz TM-15's flight was an in-orbit record for a Soyuz spaceship - 188 days 21 h 39 m.

  • 1993 February 21 - Progress M-16.  Spacecraft: Progress M. Mass: 7,338 kg (16,177 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 23 Feb 1993 20:17:57 GMT. Undocked on 26 Mar 1993 06:50:00 GMT. Redocked with Mir on 1993-03-26 07:06:03 GMT. Final undocking on 1993-03-27 04:21:00 GMT. Destroyed in reentry on 27 Mar 1993 10:25:00 GMT. Total free-flight time 2.33 days. Total docked time 31.32 days.

  • 1993 March 15 - Mir News 165: Mir-DAILY ROUTINE. 

    After the docking of freighter Progress-M16 the crew continued their reparation and replacement work on the systems of the complex. They did not much experimental work apart from geophysical observations. They needed all their working time for technical maintenance. They repaired a number of gyrodynes and Manakov was positive about the results of that 'high priority' work. I hope that I was right for Manakov is a great optimist. The VDU (the external movements control motor in the Sofora- girder) is still unserviceable due to software problems. Of great concern for crew and experts remain the complicated systems to maintain the climate in that what is like an 'iron lung'. In contradiction to the 'iron lungs' for medical use this one has to feed and regenerate itself. Wear of parts of that complicated complex results in malfunctioning, so the crew repeatedly gets warnings about hitches, but also by more noise than originally had been foreseen. Daily they speak about the BKV-3, a system to restore the condition of the air. When the crew gets permission to switch that system off (getting the command G-24), they enjoy the silence. Polishchuk did a lot of repair work on that BKV-3.

    EXTRA VEHICULAR ACTIVITIES (EVA-S):

    Shortly we can hear the crew speak about preparations for a series of 4 EVA-s. For the 1st one the 16th of April has been mentioned. During the first 3 EVA-s the cosmonauts will have to replace the solar panels from the Kristall module to the Kvant-1. The 4th one is for the removal of materials which for a long time had been exposed to the influences of open space. The solar panels have to be replaced to make future operations possible. To execute the planned docking operations of Buran and Space Shuttle to that Kristall module it has to be redocked to the forward axial (PKhO) docking port. A second reason to replace those solar panels is the fact that some solar panels hinder other ones. Daily the crew has to economise the power consumption of the complex. Polishchuk is responsible for that and in Manakov's opinion he is an expert in that field.

    MODULES:

    Possibly the plans for the launch of the Modules Priroda and Spektr have been altered. The first Module to be launched for a docking with Mir should be a technological one. So Priroda is 2d on schedule. This is a pity for Priroda is ready for launch.

    RETURN CAPSULES: Progress-M16 does not carry such a capsule and the use of such a container from Progress-M17 has not been planned. The return capsules are for 100% reliable, but due to the little amount of freight to be brought back, return capsule operations are too expensive.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1993 March 31 - Progress M-17.  Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Conducted docked and undocked longevity spacecraft longevity tests. Docked with Mir on 1 Apr 1993 05:16:18 GMT. Undocked on 11 Aug 1993 15:36:42 GMT. Destroyed in reentry over the South Atlantic on 3 Mar 1994 03:28:00 GMT. Total free-flight time 204.56 days. Total docked time 132.43 days.

  • 1993 April 19 - EVA Mir EO-13-1.  Spacecraft: Mir.

    Began installation of Kvant 1 solar array drive unit.

  • 1993 May 19 - Mir News 174: Progress-M18. 

    Launch postponed.

    During checks of the Soyuz-carrier rocket, which had to launch Progress-M18 for a flight to the space station on 19 May 1993, experts discovered a technical deficiency. They decided to postpone the launch. At the earliest the launch is possible on 22 May 1993. If so, the launch will take place at abt. 0640 UTC that day.

    Progress-M18's cargo is essential for the execution of the planning for this and next year. In the first place it has to deliver the replacement of the lost key (or: handle) for the operations with the crane Strela. During the next planned spacewalks the crew needs that Strela for the transfer of the solar panels from Kristall to Kvant-1. Progress-M18 also will bring new equipment and spare parts for the replacement or repairs of worn-out systems, but also equipment and experiments to be used during the French expedition 'Altair' in July this year.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 May 22 - Progress M-18.  Spacecraft: Progress M. Mass: 7,348 kg (16,199 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Last launch using Soyuz-U2 launch vehicle. Docked with Mir's front port on 24 May 1993 08:24:44 GMT. In addition to other supplies, carried repair equipment for a spacewalk device damaged a month before. Undocked on 3 Jul 1993 15:58:16 GMT, with Soyuz TM-17 docking at the same port only minutes later at 17:45 GMT. Meanwhile, Progress M-17 remained docked to the Kvant rear port on a longevity test. Progress M-18 was destroyed in reentry on 4 Jul 1993 17:13:00 GMT. Total free-flight time 3.12 days. Total docked time 40.31 days.

  • 1993 June 18 - EVA Mir EO-13-2.  Spacecraft: Mir.

    Completed installation of Kvant 1 solar array drive unit.

  • 1993 July 1 - Soyuz TM-17.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-14. Carried Vasili Tsibliyev, Alexander Serebrov, Jean-Pierre Haignere to Mir; returned Serebrov, Tsibliyev to Earth. Progress M-18 undocked from Mir's front port at around 17:25 GMT on July 3, and Soyuz TM-17 docked at the same port only 20 minutes later at 17:45 GMT.

  • 1993 July 1 - Mir News 177: Soyuz-TM17 launched from Baykonur. 

    On 1 July 1993 at 1433 UTC the transport ship Soyuz-TM17 was launched for a flight of 2 days to the Mir Space station. The first crew had been chosen and so Soyuz-TM17 was manned by Tsibliyev, Serebrov and the Frenchman Haignere. The French women cosmonaut Claudie Andre-Deshays will have to wait until 1996 for her flight on board the Mir station to conduct experiments of the French program Cassiopea. 3 Hours after launch Soyuz-TM17 came in our range (orbit 3, 1734 UTC) and strong signals of the 5 transmitters could be monitored (922.755, 165.873, 166.130, 166.140 and 121.750 mc). Tsibliyev reported that all was normal and that health and mood of the crew were excellent. They already had taken off their spacesuits and had just entered the 'life-compartment'. At 1656 UTC they had re-oriented their ship. This crew uses the call 'Ceres', so respectively Ceres-1, Ceres-2 and Ceres-3. So Haignere is 'Ceres-3'. During his return flight on 22 July 1993 he will be a member of Manakov's crew, the Vulkans, and then Haignere will use the call 'Vulkan-3'. During the pass in orbit 4, 1903 UTC, Tsibliyev reported all details about the 2nd orbit correction, which was executed during that pass. All went as scheduled. This had been also the case with the 1st orbit correction. Tsibliyev reported details about this correction as well for during that correction Soyuz-TM17 was out of range of tracking stations. Among the reported data were the times (in seconds) during which the S.K.D. (engines) worked, the gained speed in M/sec, the so called SIRT (fuel consumption in KG) and some pressures in tanks. During the pass in orb. 5 (2036 UTC) again radio traffic loud and clear. During the next pass the cosmonauts slept. At 221345 UTC Soyuz-T17 could be seen passing the TCA as a clear star in elevation 39 degrees. On 2 July 1993 Soyuz-TM17 will be flying autonomously. She will pass at abt. 30 minutes after Mir. Towards midnight Soyuz-TM17 as well as Mir can be observed visually if weather conditions are good. Docking can be expected on 3 July 1993 between 1615 and 1620 UTC, so not long after the first pass of both objects. If the Russians will stick to previous plans the freighter Progress-M17 will undock under observation of the approaching S- TM17. Soyuz-TM17 will dock to the docking port from where Progress-M17 undocked.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 July 4 - Mir News 178: Soyuz-TM17 docked to Mir space station. 

    This ship with on board the relief crew and the Frenchman Haignere docked to Mir (forward docking port) on 3.07.93 at 1624 UTC. The docking took place in the automatic mode (Kurs-system). Before Soyuz-TM17 began her final approach the freighter Progress-M17 had to undock. So a few minutes before the final approach Progress-M17 undocked and was brought in a safe distance from Mir. This happened before Mir, Soyuz-TM17 and Progress-M17 came in our range. During the pass in orb. 42169, 1607-1612 UTC, radio traffic could be monitored on 121.750 mc and 143.625 mc. Serebrov reported that he would obey the order to go into the landing module immediately. Neither of the crews commented the final approach. There had been a long transmission via Altair, which ended a few minutes before docking. Good images of the complex (by Soyuz-TM17's cameras) and the docking port could be seen. During the pass in orb. 42170, 1742 UTC, it was obvious that all was well: the hatches had been opened and the first meeting between the 2 crews had already taken place. Mir started to transmit to TsUP the video recordings of the approach and the welcome of the new crew. All cosmonauts, also Tsibliyev, Serebrov and Haignere, could be heard via 143.625 mc. During this pass Mir also transmitted on 145.550 mc. Via the digital memory microphone Polishchuk could be heard with a greeting of P. and Manakov to a conference of radio-amateurs in (probably) St. Petersburg. During the next pass (orb. 42171, 1915 UTC, Mir transmitted on 145.550, 143.625 and 144.475 mc. After a CQ-call in Russian and English, Haignere spoke in French with the radio-amateur Francis, FC1OKN.

    Altair: From 4.07 until 22.07.93 Haignere, in co-operation with his Russian colleagues, will conduct experiments in the framework of the French scientific program Altair.

    Spacewalks: If all goes according to previous planning the new crew (the 14th main expedition to the Mir station) will make 3 spacewalks.

    Progress-M17: This freighter still flew autonomously in the night from 3 to 4.07.93 and was visually observed by Mr. Wim Holwerda (Working group artificial satellites) during Mir's pass in orb. 42174, 2227 UTC, at abt. 8 KM behind Mir. Wim also saw the 3d stage of the rocket which gave Soyuz-TM17 the last 'push' on 1.07.93. Progress-M17 carries a return capsule. In a next Mir-report I hope to tell somewhat about the fate of Progress-M17 and that capsule.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 July 15 - Mir News 179: MISSION ALTAIR. 

    This French scientific mission goes according to plan. Haignere stated that all experiments are going well. The only problem is the fact that they have a lot of work to do. On 14.07.93 due to their work a direct TV-report in which a conversation with President Mitterand had to be cancelled or did not take place due to lack of comm. channels. H. is feeling well. No space sickness, no headache or other pains, he sleeps well and has a good appetite. H. praises the good amicable sphere among the crew members, which guarantees a good co-operation. H., call F6Mir, enjoys the possibilities of radio-amateurism: as soon as France is in range he has long conversations with French radio-amateurs. On 11.07.93 in orb. 42293, 1324 UTC, he also got the opportunity to speak with his parents. He had to ask one of the amateurs to leave the frequency (144.475 mc) for he was not able to hear his mother. On this frequency also a lot of P/R traffic. H.'s presence on board Mir caused a remarkable increase of French amateur-calls on Mir's P/R.

    Mir-crew: Manakov is still captain of the Mir-complex and this he shows clearly. During every pass he tightly holds the microphone. Now and then Polishchuk and Serebrov can be heard; Tsybliyev, who has to take over command one of these days, rarely speaks with TsUP.

    Progress-M17: During the experiment 'Rodeo' on 3.07.93 this freighter undocked from the Mir station while Soyuz-TM17 was waiting for the docking port freed by Progress-M17. Progress-M17 undocked at 1553 UTC. Soyuz-TM17 docked to Mir at 1624 UTC. The return-capsule of Progress-M17 landed safely in Kazakhstan at 1802 UTC.

    Soyuz-TM16: With this ship, now still attached to the Kristall- Module, Manakov, Polishchuk and Haignere will return to earth on 22.07.93. The landing is expected at about 0630 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 July 16 - Mir News 180: Movements of Progress-M's and Soyuz-TM's. 

    Movements of Progress-M's and Soyuz-TM's in the near future:

    Progress-M18: Will undock from Mir and decay in the atmosphere on 24.07.93 (so 2 days after the departure of Soyuz-TM16).

    Progress-M19: Launch from Baykonur on 27.07.93.

    Progress-M20: Launch from Baykonur on 12.10.93.

    Soyuz-TM18 : Launch from Baykonur with crew Afanasyev and Usachov on 16.11.93.

    Progress-M21: Launch from Baykonur on 30.11.93.

    In May 1994 there will be a flight of a Soyuz-TM to Mir with on board Malenchenko and Strekalov. (Strekalov replaced Kaleri, because he has more experience than Kaleri.) The 3d crew member will be a physician for a long duration flight of one and a half year. For this flight 3 physicians are selected, one of them will fly, namely Polyakov, Arzamazov and Morukov.

    The Russians have the intention to launch Module Spektr on 20.12.93 for a flight to Mir. This long expected extension will be welcomed by the crew of the 15th Main expedition to Mir: Afanasyev and Usachov.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 July 22 - Mir News 181: Soyuz-TM16. 

    SAFE AND SOFT LANDING AT 064200 UTC.

    Soyuz-TM16 landed safely in near the city Dzhezkazgan in Kazakhstan. The ballistic section of Professor Ivanov again deserves admiration for their excellent work: the landing took place 23 seconds later than calculated. During this flight the crews of Mir and Soyuz-TM16 as well had to do somewhat extra in this field for at the moment of undocking the objects were out of range of NIP (measurement points on earth). So they had to take care for the actual attitudes during undocking and thereafter. Data for this operation they got during radio traffic with TsUP on 21.07.93. Just after the separation of the Life compartment (BO) and the Motor block from the Landing module (SA) the SA entered the dense layers of the atmosphere at 061817 UTC surrounded by the fire of the plasma. At a distance of appr. 400 KM the crew on board Mir was able to observe this through porthole nr. 9. At 062655 UTC the main parachute opened and the landing took place at 064200 UTC. So the crew of the 13th Main expedition to Mir, Manakov and Polishchuk, and the French 'spacionaute' Haignere accomplished their flights. H. was able to execute the French scientific program Altair. The last days of his flight he felt tired due to the huge amount of work, which was necessary to get a maximum profit of such an expensive flight. H. was very satisfied about his work on board but also about his activities as a radio- amateur and he was very grateful to make a lot good QSO-s with French and other amateurs.

    Mir: On board Mir are now the cosmonauts Tsybliyev and Serebrov. Their official calls are not 'Ceres' as has been published earlier, but respectively Sirius-1 and 2. Their calls for radio- amateur activities are resp. R3Mir and R4Mir. Ts. en S. will work in open space 3 times in September this year to accomplish the transfer of the solar batteries from the Kristall-module to Kvant-1.

    In a next Mir-report I hope to give attention to the last days of the presence of 5 cosmonauts on board Mir.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 July 22 - Landing of Soyuz TM-16. 

    Soyuz TM-16 landed at 06:41 GMT with the crew of Haignere, Manakov and Polishchuk aboard.

  • 1993 July 26 - Mir News 182: Ham-work during successfully accomplished Altair mission. 

    Jean-Pierre, F6Mir, was an enthusiastic and skilled amateur. In this field he did not yield to Tognini during his flight in 1992. H. made all his QSO-s in the proper way and during the last day of his flight he told in a CQ-message that he had been pleased by radio-amateurism and he expressed his gratitude to all amateurs with whom he had been in contact. He was not pleased about an Italian amateur, who, using a very strong signal, often blocked the uplink too long. He limited H's possibilities to make more QSO-s with French and other amateurs.

    Mir-crews: On 16.7.93 the control over the Mir-station had been transferred to the new crew: Tsibliyev took care of the attitude control and Serebrov had replaced Polishchuk as board-engineer. Manakov and Polishchuk prepared their return flight. Their main concern was to find room in Soyuz-TM16 for all what they had to bring back to earth. Thoroughly they checked the on board systems of that ship and rehearsed the procedures for the navigation during and after the undocking from Mir on 22.07.93. A physician at TsUP regularly checked the health of M. and P.

    New crew: As of 22.07.93 Tsibliyev and Serebrov are working strenuously. They are busy with a lot of important repairs and replacements. Obviously they have to solve all problems with the attitude(movements-) control of the complex. (Gyrodynes and the VDU motor in the Sofora-girder). They already work on the Gyrodynes. It is a pleasure to hear the new crew: undoubtedly excellent cosmonauts. Quite normal for S.: this is his 4th flight, but the novice T. acts as if he has a long experience in space.

    Progress-M18 and M19: Recently the decay of the first freighter (M18) still was on schedule for 24.07.93. This has been put back. Though still not for 100% sure the plan is to undock Progress-M18 on 8.08.93 after the launch that same day of Progress-M19. If this happens it will be a novelty: for a while 2 freighters flying autonomously in space.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 August 6 - Mir News 183: Exchange of freighters. 

    Progress-M19: The launch date of this freighter for the Mir station has been put back for the 2d time. Now this launch from Baykonur is planned for 10.08.93 at 2216 UTC (for the Russians already on 11.08.93 at 0116 TsUP time). If all goes according to the plan Progress-M19 will dock to Mir at abt. 0000 UTC on 13.08.93. So a few minutes after the first pass of the Mir complex on (for us still) 12.08.93 2350-2356 UTC, pass in orbit 42799. Progress-M19 will dock to the forward port (transition section P.Kh.O.). This port is still occupied by the Progress-M18.

    Progress-M18: This ship will separate from Mir and decay in the atmosphere if the launch of Progress-M19 is successful.

    Radio-amateur traffic new crew: The new crew has not been heard with amateur traffic (packet radio or phone) on the known amateur frequencies during passes within our range. The crew asked TsUP for a computer program to clean the overloaded memory of their computer, which contains a lot of correspondence and documents of the previous crew. So possibly they will resume packet-radio after the deletion of all superfluous files. During a packet QSO with TsUP on 143.625 mc Mir used the call R0Mir.

    Spacewalks (EVA-s): The 3 EVA-s planned for September 1993 have been cancelled. The present crew (14th Main expedition) will not carry out any EVA-s.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1993 August 10 - Progress M-19.  Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir at the Kvant rear port on 13 Aug 1993 00:00:06 GMT. Undocked on 13 Oct 1993 17:59:06 GMT. Destroyed in reentry on 19 Oct 1993 00:22:14 GMT. Total free-flight time 7.33 days. Total docked time 61.75 days.

  • 1993 August 11 - Mir News 184: Progress-M19. 

    This freighter has been launched from Baykonur on 10.08.93 at 2223 UTC (for Moscow and TsUP-time already 11.08.93) for a 2-days flight to the Mir-station. Perhaps there has been a slight delay for I expected the launch at 2216 UTC. Somewhat later than expected I monitored the transmissions of Progress-M19 on 922.755 mc and in the 166 and 165 mc bands between 0256 and 0301 UTC. To enable Progress-M19 to dock to the forward docking port of Mir (transition section P.Kh.O.) the old Progress-M still docked to that port has to disappear soon. This undocking is scheduled for 11.08.93 at 1534 UTC.

    Perseid-meteorites: These meteorites coming from the comet Swift- Tuttle are visible (clouds permitting) around 12 august every year. Thus far clouds did not permit this for us this year, but the Mir-cosmonauts, not hindered by clouds or fog, were able to see the meteorites. Tsibliyev, the captain of the Mir-station, reported during the pass in orbit 42770, 11.08.93, 0452-0503 UTC, that they saw a little bit of it. He added that he had to report some 'battle wounds'. He told TsUP that the station had been hit by 4 particles obviously coming from that meteorite-rain. They caused minor damages to 2 solar batteries (on the base block and on Kristall - Module-T) and to one of the portholes. The window of that porthole showed a cavern with a diameter of 2 a 3 mm. T. nor TsUP did not show any concern. To be realistic: thus far we have to do with minor particles, but bigger particles can cause serious damages to space-ships and stations, even leakage and consequently decompression. In my opinion the recent experience of the Mir-crew fully justifies NASA's decision to put back the launch of Space shuttle Discovery until 12.08.93 due to concern for that meteorite-storm.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 August 13 - Mir News 185: Progress-M19 docked to Mir-space station. 

    This freighter with food, water, fuel, post, spare parts, etc. docked to the forward docking port transition section -P.Kh.O.) on 13 Aug. 1993 at 0000 UTC. So 4 minutes after LOS for our position. The approach in orb. 42799, 12 Aug. 2351-2356 UTC, the cosmonauts visually observed the Progress-M19. At 2356 UTC Progress-M19 was on a distance of 25 M and the appr. speed was 0.85M/sec. The operation passed off smoothly and already during the pass in the next orb. (42800, 0129-0133 UTC) Tsibliyev reported the hermetic air-seal and the opening of the hatch to Progress-M19. In the pass during orb. 42801, 0304-0309 UTC, the cosmonauts expressed their gratitude for all what Progress-M19 delivered, but in Serebrov's opinion the Progress-M19 was 'too empty'. He said that only 66% of the cargo-volume had been utilised. Nevertheless he was satisfied about the post, the new paper (or: ribbon) for the RTTY printer and the renewed instructions for evacuation in case of emergency.

    Perseid-meteorites: So the crew just had to work during 3 night shifts: 2 due to the meteorite-storm and 1 for the Progress-M19. In the night from 11 to 12 Aug. they enjoyed the sight of the meteorite-rain. They spoke about 'fireballs' and stopped counting them for it really was a rain. The night before they also observed this phenomenon, which was less spectacular then. Unfortunately they again had to report collisions with small particles and damages. S. and T. expressed their relief that all was over now and that they survived the meteorite-bombardments.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 September 14 - Mir News 186: SPACE-WALKS (EVA-S). 

    Some weeks ago TsUP announced that the 3 EVA-s, which had been planned for Sept. this year had been put back and that this crew (the 14th main expedition to Mir) would not make any EVA-s at all. Later on there happened to be a plan to execute an EVA on 10.09.93. This EVA has been put back also. Meanwhile it was obvious that 1 or more EVA-s are badly needed for the inspection of the outer surface of the whole complex. Experts even considered the use of the SPK (MMU) for EVA-s. Board- engineer Serebrov knows how to fly with the SPK: he was the first cosmonaut to fly with it on 1.02.90. Radio traffic during recent passes revealed that the crew is preparing an EVA. Whether they will use the SPK or not is not clear.

    CONSEQUENCES OF THE PERSEID METEORITE STREAM ON 12.08.93:

    After a long period of silence the Russians officially admitted that the station suffered from hits caused by minuscule particles during the Perseid-meteorite stream. One hit even caused a hole in a solar battery with the diameter of appr. 6 cm. Meanwhile messages and questions about the damages reached the Mir crew by amateur radio. Experts are evaluating the eventual influence of the damages on the power supply of the complex. The crew cannot see the whole outer surface of the station from inside and so EVA-s must be carried out to inspect it thoroughly.

    RADIO-AMATEUR TRAFFIC:

    For some weeks again a lot of Packet radio tfc on 145.550 mc. Sometimes there are also calls by 'phone' on that frequency. On 12 and 13.09.93 the crew used 145.500 mc to contact the Irish amateur EI3SI by speech.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 September 16 - EVA Mir EO-14-1.  Spacecraft: Mir.

    Began installation of Rapana truss.

  • 1993 September 17 - Mir News 187: First spacewalk (EVA) cosmonauts Mir. 

    Tsibliyev and Serebrov executed their first EVA on 16.09.93. At 0435 UTC they crawled in their spacesuits and at 0604 UTC they opened the exit hatch. After an EVA of appr. 4 hrs 16 mins they closed that hatch behind them. And again this time a change in previous plans: so not as expected, the inspection of the outer surface of the complex or the transfer of the solar batteries from the Kristall-module to the Kvant-1. This time they prepared the installation at the base of the Sofora-mast of a truss structure, called Rapana. The Rapana uses the design for the construction of support arms, which will be used for Mir-2 or for Mir-2's integration in the international station Freedom. The Rapana has a length of several meters and a cylindrical shape. For the installation of this Rapana 3 EVA's are needed, the 2d one will be executed on 20.09.93. It is still unknown when there will be an EVA for the inspection of the outer surface of the complex or whether that inspection will be done during the 2d or 3d EVA. After the installation the Rapana will serve as a platform for experimental materials to be exposed to the influence of open space.

    Another EVA on 16.09.93:

    The astronauts of the space shuttle Discovery also executed an EVA this day. About this EVA the Western media brought news and images, which they did not about the Russian EVA. And that is why I did!

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 September 20 - EVA Mir EO-14-2.  Spacecraft: Mir.

    Completed installation of Rapana truss.

  • 1993 September 20 - Mir News 188: 2d Spacewalk (EVA) Mir-Crew. 

    Tsibliyev and Serebrov concluded the installation of the Rapan pillar during a relatively short EVA on 20.09.93 between 0352 and 0705 UTC, so 3 hrs and 13 mins. The Rapan is standing perpendicularly on the Kvant-1 module near the Sofora mast. The Sofora is standing under an angle of 79 degrees and inclines towards the forward side of the complex. The crew installed materials, samples and equipment on the Rapan for an exposure to open space during half a year. After this period the samples etc. have to be returned to earth for analyses.

    Eventual 3d EVA:

    After evaluation of today's EVA and an analysis of the TV-images made by the cosmonauts, experts will decide whether there will be needed a 3d EVA. The Russians did speak nor about the inspection of Mir's outer surface and the solar batteries neither about the transfer of solar batteries. If a 3d EVA will be made, this might be on 24.09.93.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 September 22 - Mir News 189: 3d Spacewalk (EVA) put back. 

    Until 22.09.93 the cosmonauts made preparations for an EVA on 24.09.93. During that EVA they had to execute the program 'Panorama', which is an inspection of the outer surface of the station by camera's. On 22.09.93 TsUP announced that the EVA had been put back to 28.09.93. A reason for the delay has not been stated. Possibly the unstable political situation in Moscow has something to do with it, but technical reasons are also possible. On 22.09.93 the crew worked on a problem with a pressure-valve (KVD) of the airlock (Sh.S.O.) in Module-D.

    Mir-station hit by a particle from outer space:

    On 21.09.93 at abt. 1205 UTC, while the station was near the equator, Tsibliyev heard the clap of a particle colliding with Mir's outer surface. The impact caused a little cloud of dust and released some pieces of paint of the wall. Tsibliyev heard the impact while he was flying from Kvant-1 to the Base Block. Serebrov, who was working in Module-D, did not hear it.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 September 28 - EVA Mir EO-14-3.  Spacecraft: Mir.

    Installed material samples and retrieved experiment packages. Documented external condition of Mir.

  • 1993 September 28 - Mir News 190: 3d Spacewalk (EVA) Mir crew. 

    The crew of the 14th Main Expedition Mir made their 3d EVA on 28.09.93. Planned had been a long EVA (4 or 5 hrs). The crew opened the hatch of Module-D's airlock at 0057 UTC. They had to return after 1 hr 51 mins due to a malfunction in the thermoregulation of commander Tsiblieyev's spacesuit. So they closed the hatch behind them at 0248 UTC. TsUP considered to continue the EVA by Serebrov alone, but 'safety first' prevailed and both cosmonauts concluded the operation at 0248 UTC. So they could not execute the whole plan for this EVA. Main task was the experiment Panorama, an inspection of the outside elements of the station by photo- and video camera. They partly fulfilled this task. The second task was the collection of the American experiment TREK. Serebrov removed the unit in which samples and materials had been exposed to open space for a long time and brought this back on board. In the near future this experiment will be brought back to earth for analyses by the American scientists. Communications during this EVA took place via Altair and after the EVA at 0439 UTC Mir and TsUP communicated again via VHF. The cosmonauts felt well and during the passes in the orbits 43521 until 43523 they already spoke about other matters. There might be a 4th EVA, but this has not been decided so far.

    Reason delay transfer solar batteries from Kristal to Kvant-1:

    Several times this work has been put back. Reason for this delay at the moment is the fact that the launches of the modules Spektr and Priroda to Mir have been delayed due to financing problems. The Russians hope to get support from the west, where a lot of scientists are convinced of the scientific value of those modules.

    Progress-M20: The launch of this freighter is still on schedule for 12.10.93. The crew is already involved in the loading of Progress-M19 with goods they have to get rid off and cargo for the Ballistic Return Capsule (VBK).

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1993 October 8 - Mir News 191: Progress-M17. 

    This freighter undocked from Mir after the launch of Progress-M19 on 10.08.93. (So this happened not to be the Progress-M18. Progress-M18 disappeared earlier, i.e. just after the Rodeo- experiment. (Undocking of Progress-M18 under observation of the approaching Soyuz-TM17 which had to dock to the docking- port freed by Progress-M18). While Progress-M19 was flying to Mir Progress-M17 undocked and remained in space. The autonomous flight of this freighter will have a duration of 1 or 1.5 year. This on request of the Americans, who plan to use modified Soyuz-M-ships as ACVR-s (assured crew rescue vehicle) for their space stations. They wish to know the maximum lifetime of a Soyuz-TM. Most of the systems of both vehicles are equal and so Progress-M17 is now playing the role as a test-vehicle. Progress-M17 is flying a dozen kilometres lower than Mir.

    Mir-operations:

    The still attached to Mir Progress-M19 corrected the orbit of the complex. Mir was lifted from ap/per 390.7/384.8 KM to ap/per 397.4/389.2 KM. So Keplers older than day 278 are invalid. The crew still has to spend a lot of time to keep the life systems of the complex operational, especially the water regeneration systems cause a lot of trouble. On 7 Oct. 1993 during their first contact with TsUP (in orb. 43660, 0535-0546 UTC) they heard that the launch of the Soyuz-TM18 with the relief crew had been put back until the 2d half of December 1993 (instead of 24.11.93), which means a prolongation of their flight. The delay is caused by a complex of reasons, one of them has something to do with the carrier-rocket for Soyuz-TM18's launch. Serebrov stated that he and Tsibliyev understand this decision and that they, though reluctantly, agreed to remain longer in space. They asked TsUP to inform Yuriy Semyonov (Head of NPO Energiya) about their consent.

    PROGRESS-M19: The crew is preparing this freighter for her imminent departure. Main task is the loading and servicing of the VBK (ballistic return capsule) of Progress-M19. Progress-M19 will undock from Mir after the eventual successful launch of the freighter Progress-M20.

    PROGRESS-M20: Launch still on schedule for 11.10.93, 2133 UTC (so for TsUP already on 12.10.93, 0033 Msc Winter Time) from Baykonur. Rendezvous and docking with Mir in the late evening of 13.10.93 ( UTC).

    4th Spacewalk (EVA): This EVA will be carried out after the arrival of Progress-M20. The most convenient day for this EVA will probably be 28.10.93. Chris v.d. Berg, NL-9165/A-UK3202

  • 1993 October 11 - Progress M-20.  Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir, carried a Raduga reentry capsule for return of experimental materials to earth. Docked with Mir on 13 Oct 1993 23:24:46 GMT. Undocked on 21 Nov 1993 02:38:43 GMT. Capsule landed in Kazakhstan on 21 Nov 1993 09:06:00 GMT. Total free-flight time 2.35 days. Total docked time 38.13 days.

  • 1993 October 12 - Mir News 192: Progress-M20. 

    The launch of this freighter took place on 11.10.93 at 2133 UTC (for the Russians, using 'decree-time', already 12.10.93 0033 hrs). Progress-M20 reached the right initial orbit and the first corrections have been executed successfully. Progress-M20's transmissions in the 166, 165 and 922 bands could be monitored in the pass in the 2d orbit on 12.10.93 between 0035 and 0037 UTC. Progress-M20 has to deliver to the Mir-station spare parts, food, water, fuel and post. It contains also a package of experiments in the framework of Biokrist. These are protein-crystallisation experiments from several countries. One experiment is of Dr. Grip of the Faculty for Eye Surgery, University of Nijmegen (the Netherlands). A Biokrist container, including the same Dutch experiment, has been on board of the Mir-complex in the first 3 months of 1992. During the transport, after the skilful delivery on earth by the cosmonauts Volkov and Krikalyov, something went wrong due to extreme low temperatures and the results suffered damages. The present experiment will return to earth by the crew of this expedition in December 1993. In 2 days Progress-M20 will fly to Mir and if all goes well the freighter will dock to Mir on 13.10.93 at abt. 2316 UTC (so for the Russians already on 14.10.93, 0216 Msc decree-time).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 October 14 - Mir News 193: Progress-M20 DOCKED TO Mir. 

    This freighter docked to Mir's aft docking port (Kvant-1) on 13.10.93 at 2325 UTC. The approach and docking took place in the automatic mode under observation of the crew. The docking took place a little bit later than expected after Mir's pass in orbit 43764 from 2309-2314 UTC. During this pass the transmitters of Progress-M20 still could be monitored on 922.755 mc and in the 166 and 165 mc bands. Mir also worked with packet radio on 145.550 mc. During the passes in orb. 43765 (14.01 0043-0050 UTC) and 43766 (0221-0227 UTC) the crew and TsUP spoke about the just arrived freighter. The crew was satisfied: the ship was clean and they got the badly needed dairy-products, which they ordered only recently. Progress-M20 has a V.B.K. (ballistic return capsule) on board. The arrival of the Progress-M20 is good news for the Dutch University in Nijmegen for she safely delivered their experiments in the Biokrist-package.

    PROGRESS-M19:

    To enable Progress-M20 to dock with the complex the Progress-M19 had to disappear. Nowadays the Russians undock the old freighter as soon as they are sure about the right orbit and the good functioning of the new one. So Progress-M19 separated from Mir on 12.10.1993 at 1759 UTC. Before burning up in the atmosphere Progress-M19 jettisoned the V.B.K. and this landed safely in the designated area on 13.10.93 at 0022 UTC. The crew on board Mir did not go asleep but observed the whole operation. The were enthusiastic about this interesting event. They saw how the engines of Pr-19 worked, how the V.B.K. separated from Progress-M19 and they even could see the burning up of the rest of the freighter. They made a lot of video-films and images. During the pass in 43751, on 13.10.93 at 0135 UTC they reported about these observations to TsUP. In the course of 13.10 they transmitted their films to TsUP via the geostationary satellite Altair.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 October 21 - Mir News 194: 4th Spacewalk (EVA). 

    This EVA has been put forward and will take place on 22.10.93. The crew will open the hatch at 1630 UTC and the EVA has to last 3 or 4 hours. During this EVA the crew will conclude the experiment Panorama. This is an inspection with camera's of the outer surface of the complex. Special attention will be given to the damages caused by particles from outer space during the Perseid meteorites storm around 12.08.93 and that of the collision with something from outer space on 21.09.93. Serebrov will execute this survey from a position in the top of the Strela crane (or: girder). The crane will be steered by Tsibliyev.

    Progress-M20:

    This freighter will undock from the complex on 21.11.93. After jettisoning the V.B.K. (return capsule) Progress-M20 will burn up in the atmosphere. The undocking and decay of Progress-M20 has been put forward due to one of the American (Boeing) experiments. To keep this experiment in space until the return of Soyuz-TM17 to the 2d decade of January 1994 was undesirable.

    Reason for the delay of the launch of Soyuz-TM18:

    This delay has been caused by the bad economical situation. Simply: there was no funding available for a launch in November 1993. Soyuz-TM18 will start on 4.01.94 with the relief crew (15th main expedition to Mir) on board. One of the crew of 3 persons will be a doctor (Polyakov or Arzamazov), who will remain on board Mir for 1.5 year. The present crew (14th main expedition) will return to earth with Soyuz-TM17 on 12.01.94, so their flight will last well over 1.5 months longer than foreseen in the original planning. Though reluctantly Tsibliyev and Serebrov agreed to this delay.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1993 October 22 - EVA Mir EO-14-4.  Spacecraft: Mir.

    Retrieved micrometeoroid detectors.

  • 1993 October 23 - Mir News 195: 4th Spacewalk (EVA) Mir-crew on 22.10.93. 

    This EVA started earlier than was expected. The hatch swung open at abt. 1535 UTC. During the first half hour of this EVA the cosmonauts spoke with the Russian premier-minister Chernomyrdin who visited TsUP. Regretfully this EVA ended earlier than planned due to a malfunction of a life system Serebrov's spacesuit. The EVA took place between (plus/min) 1535-1615 UTC and had a duration of only 38 minutes. The crew succeeded in installing on the outer surface of the complex a device for measurements of the micro-meteorite flux and the salvaging of materials which had been exposed to the influence of outer space. Serebrov made some images in the framework of the Panorama experiment, but for the conclusion of that experiment another EVA will be necessary. Our good friend OM Peter observed via Altair that the cosmonauts had left the airlock. After a while the transmission of images switched over to the system Orbita and only the speech could be monitored. Soon we derived from this traffic that the cosmonauts were in the airlock, that they had closed the exit hatch and were equalising the pressures between the airlock (S.Sh.O.) and the instrument- and scientific compartment (P.N.O.). For that purpose they had opened the valve K.V.D. and via the downlink the sound of streaming air could be heard. During the first pass within VHF-range (in orbit 43902, 1932- 1937 UTC) the cosmonauts reported that all was well. The possible date of the 5th EVA also was mentioned. This might be 29.10.93 depending on further analyses of the emerged problems.

    Information: The English service of Radio Moscow slightly paid attention to this EVA, but did not speak about the cause of the premature return on board of the crew. For the first time in the history of spaceflight Radio Moscow spoke about the Russian crew as 'astronauts' instead of 'cosmonauts'.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 October 29 - EVA Mir EO-14-5.  Spacecraft: Mir.

    Installed equipment on exterior of Mir

  • 1993 October 30 - Mir News 196: 5th Spacewalk (EVA) Mir-crew on 29.10.93. 

    The crew opened the hatch at 1338 UTC and closed this behind them at 1750 UTC, so the duration of this EVA was 4 hrs and 12 mins. They fully accomplished their tasks: the experiment Panorama, during which Sererbrov made video-images of the outer surface of the station, they removed samples of materials which had been exposed to open space and placed new samples and on instructions from experts on earth they carried out an inspection of objects on the outside, for instance the solar panels. They also carried out prophylactic work. Most of the radio-communications was relayed by the satellite Altair. During the first 2 passes for our position the EVA was still going on and the radio-traffic could be heard on VHF as well as on Altair. During the pass in orbit 44010, 1742-1752 UTC, the cosmonauts returned to the airlock and they told TsUP that they were ready to close the hatch on TsUP's command. So they did at 1750 UTC and they immediately started with the equalisation of the pressures between the airlock (S.Sh.O.) and the Instrument-Scientific compartment (P.N.O.). OM Peter monitored phone as well as TV-images and in co-ordination with him I was able to determine that all went well during this EVA. During the first communication session via Altair after the EVA the cosmonauts transmitted images made during the EVA to TsUP. So OM Peter could see how the crew during their EVA jettisoned an old (probably no longer usable)EVA or spacesuit. They succeeded in sending away this dummy in such a shape that it looked like someone who saluted like a soldier. After analyses of the monitored radio-traffic I hope to tell something about the crew's assessment of the damage, which had been caused by micro-meteorites around 12.08.93.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 November 16 - Mir News 197: Progress-M20. 

    For some time the Mir-crew is preparing the freighter Progress- M20 for its last autonomous flight. They store all what they want to throw away in the Progress-M20 herself and all experiments, films etc. in the return capsule (VBK). The Progress-M20 has to undock from Mir on 21.11.93 at abt. 0900 UTC for decay in the atmosphere. Before burning up the Progress-M20 will jettison the VBK for a safe landing in the Orenburg region, so on Russian territory. A landing in Kazakhstan means that the Russians must pay import duties to Kazakhstan!

    Orbit correction: One of these days the Progress-M20 will have to correct the orbit of the complex. After this correction old Keplers will no longer be valid.

    Mir-crew: The cosmonauts reported that the outside surface of the Mir-station is in a good shape. The damages caused by micro- meteorites are not that bad as previously expected. More concern they expressed about the inside systems of the station. The guaranteed lifetime is running to its end and they have to do a lot of strenuous maintenance work on the life systems. Nowadays they have problems with the provision of oxygen.

    Contact between Mir and Shuttle Columbia on 26.10.93:

    It was a great surprise for the Mir-crew to get a call in Russian from the Columbia on a radio-amateur channel.

    Renovation work in my shack:

    Due to renovation work in my shack it might be difficult to maintain my operational possibilities for a while. So there might be a period in which I will be unable to make Mir- reports. Please don't worry: when this misery is over I will be back again!

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1993 November 21 - Mir News 198: Progress-M20. 

    Orbit correction: On 17.11.93 during orbit 44300 the engines of Progress-M20 corrected the orbit of the Mir-complex: Ap/per now 395.3/388.2 KM.

    Decay of Progress-M20 and safe landing return capsule on 21.11.93:

    Undocking of Progress-M20 from Mir at 0236 UTC. Progress-M20 jettisoned the VBK (return capsule) at 0850 UTC. Progress-M20 entered dense layers of the atmosphere at 0851 UTC and decayed. The VBK safely landed not far from Orsk at 0903 UTC. Orsk is a town just north of the border with Kazakhstan. The VBK itself landed just inside Kazakhstans territory. So possibly Russia will have to pay Kazakhstan import duties for the VBK and the cargo.

    VBK's cargo:

    The cargo mainly consisted of 2 American containers with experiments: The first one is the experiment TREK, which had been installed outside Mir from 4.04.91. This experiment registered particles of super-heavy elements in the cosmic radiation. The 2d American experiment was the grow of biological crystals delivered by the firm Boeing. The VBK brought back to earth some Russian experiments: 2 videocassettes with images made during the survey experiment Panorama, an experiment with Ultraviolet in the earth's atmosphere, a sample of thermo-insulation material exposed to open space and a lot of negative-films.

    Progress-M21: It is still unknown when this freighter will be launched for a flight to Mir. This freighter is badly needed, especially for a supply of fresh oxygen. The last days the crew is complaining about problems with the air pressure and oxygen, which cause respiration problems (dry nostrils and throat).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1993 December 10 - Mir News 199: Progress-M21. 

    For a long time we expected the launch of the freighter towards the end of November 1993. Due to economic and other problems this launch has been put back. The launch is now on schedule for 26.01.1994, so long after the relief of the present crew.

    SOYUZ-TM18:

    This ship will be launched for a flight to the Mir-station on 6.01.1994. If all goes according to the original planning the relief crew will consist of 3 cosmonauts. One of them is a doctor (Polyakov or Arazamov) who must remain in space for 1.5 year. Whether the crew will consist of 2 or 3 cosmonauts is not sure for 100%.

    Mir-routine:

    In this period Mir's passes are in the night hours. The crew is still busy in keeping the station operational. They have to pay a lot of attention to the life-support systems: air pressure- and air composition and the water regeneration systems Elektron and S.R.V.-U.

    Visit of the American vice-president to TsUP:

    The Russians very badly need financial support from the United States for the upgrading of the partly worn-out Mir-station. So they are very pleased that vice-president Gore will visit Kaliningrad near Moscow around 14.12.93. He will also visit the flight control centre TsUP.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 January 6 - Mir News 201: Soyuz-TM18. 

    The launch of this ship with the relief crew of 3 will take place from Baykonur on 8.01.94 at 1005 UTC. If all goes according to schedule Soyuz-TM18 will dock to Mir on 10.01.94 at abt. 1148 UTC.

    Soyuz-TM17:

    The present Mir-crew (Tsibliyev and Serebrov) is already involved in activities related to their oncoming relief and their return to earth on 14.01.94. On 5.01.94 they remained on board of this ship for a long time to check systems and to look for areas in which they can stow things, which have to be returned to earth.

    Progress-M17:

    This freighter is still flying autonomously after the separation from Mir on 11.08.93. The Russians left Progress-M17 in space to check the lifetime of the systems due to the future use by the Americans of a Soyuz-TM modification as ACVR (rescue boat) for their space station. During a manoeuvre before Christmas the station came in a lower perigee (235 KM) due to a failure in the attitude control system. TsUP lost control over the freighter and they plan to have her decayed in the end of February this year. Probably this will happen spontaneously: the present orbital elements will lead to a decay at abt 28.03.94 (+ or - 3 days).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 January 8 - Soyuz TM-18.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-15. Docked at the Kvant module on January 10 at 11:15 GMT. Transported to the Mir orbital station of a crew comprising the cosmonauts V M Afanasev, Y V Usachev, and V V Polyakov for the fifteenth main expedition.

  • 1994 January 9 - Mir News 202: Soyuz-TM18 blasted off for flight to Mir. 

    Soyuz-TM18 has been launched from Baykonur on 8.01.94 at 1005 UTC. All went well and at 1014 UTC Soyuz-TM18 had reached the right orbit. For the flight the 1st crew had been selected, so: Captain V. Afanasyev, who makes his 2d flight, board engineer (rookie) Yu. Usachev (pronunciation Usachov ) and the physician Dr. V. Polaykov, making his 2d flight. He will try to remain 427 days in space. The call of the crew is Derbent, so resp. Derbent-1, 2 and 3. For radio-amateur traffic resp. U9Mir, R3Mir and U3Mir. Soyuz-TM18 came in range during orbit 3, 1307 UTC. Strong transmissions on the known frequencies (121.750, 165.874 and 922.755 mc). Afanasyev reported that all went well and he added some pressure values. After abt. 30 mins Mir (orb. 45114) could be heard here. TsUP told the Mir-crew that all on board Soyuz-TM18 was normal. In the pass in the 4th orbit (1436 UTC) Afanasyev reported that the Soyuz-TM18 executed 2 orbit corrections without significant problems. During the pass in the 5th orbit (1609- UTC) Afanasyev reported the successful performance of Soyuz-TM18 during the 3d orbit correction. Afanasyev got the order to adjust the Globus position indicator and Dr. Polyakov stated that the condition of the crew was excellent. On 10.01.94 at 1150 UTC Soyuz-TM18 has to dock to the Mir-complex. This will be abt 4 mins. after LOS of the space objects in Mir's orbit nr. 45144.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 January 11 - Mir News 203: Soyuz-TM18 docked with the Mir-space station.. 

    On 10.01.94 at 1050 UTC Soyuz-TM18 docked to the Mir-station. Approach and docking took place in the automatic mode by the use of the system Kurs. During Mir's pass in orbit 45144 (1138-1147 UTC) the approach was going on. Afanasyev watched the behaviour of Soyuz-TM18 on his monitor. He had to be alert to take over manually, but this was not necessary. Soyuz-TM18 approached and docked smoothly. During the approach the transmitter of Mir and of the Soyuz-TM18 as well could be heard. During the pass in the next orbit (45145, 1315-1323 UTC) the hatch was opened and the enthusiastic welcome and greetings of both crews could be monitored. The following pass (orb. 45146, 1448-1459 UTC) Serebrov spoke a word of welcome and reported that mood and health of the newcomers were excellent. For Dr. Polyakov reason to gather blood samples from the cosmonauts to be able to confirm this scientifically.

    The 5 men will work together during the next 3 days and the old crew (Mir Main expedition nr. 14) will then hand over the station to the 15th Main expedition.

    On 14.01.1994 Tsibliyev and Serebrov will return to earth in the Soyuz-TM17.

    The 15th Main Expedition will last until 6.07.1994, so 177 days. Then Afanasyev and Usachev will be relieved by Malenchenko, Musabayev and Strekalov. Strekalov will return with the relieved crew. Dr. Polyakov will remain on board until spring 1995 (427 days) to conduct medical experiments aimed at the long-lasting flights to Mars.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 January 14 - Landing of Soyuz TM-17. 

    Soyuz TM-17 landed at 08:24 GMT with the EO-14 crew of Serebrov and Tsibliyev aboard.

  • 1994 January 15 - Mir News 204: Soyuz-TM17 returned to earth. 

    On 14.01.1994 at 0819 UTC (08 hrs 18 mins 20 secs) the return capsule of the Soyuz-TM18 landed at 215 KM West of Karaganda in Kazakhstan. The cosmonauts (Tsibliyev and Serebrov) felt well after their flight of 197 days. They will be flown to Starcity near Moscow this afternoon. Again a routine-message about a routine-operation, but yet 'it has been a near thing' and nearly I had to draft a real shocking message!

    Return operation:

    At 0145 UTC the hatch of Soyuz-TM17 was closed behind Tsibliyev and Serebrov. At 0430 UTC the Soyuz-TM17 undocked from Mir. Tsibliyev had got orders to make a short inspection flight around the Mir-complex. They had to make images of the outer surface and they had to give special attention to the APAS89 docking system on Kristall (Module-T). In a distance of 30 Meters S- TM17 deviated from the desired course and collided with the Mir-station. Immediately radio contact with Soyuz-TM17 was lost. After 10 minutes TsUP managed to re-established radio contact with Soyuz-TM17 and the crew reported that their ship did not suffer damages and that the air-seal was still in good order. They also did not see any damages on the Mir-complex. Soyuz-TM17 made its last 2 orbits around the earth and the descent started at abt. 0715 UTC. At 0804 UTC the parachute opened and the 2-tonne heavy capsule made a safe landing at 08.18.20 UTC.

    Mir:

    The new crew (15th Main Expedition) immediately started observations through the portholes to try to determine eventual damages. During the passes in orbits 45206 (1100 UTC) and 45207 (1234 UTC) they transmitted to earth video-images which they made during the departure and fly-around of Soyuz-TM17. Shortly Afanasyev and Usachov will have to make a non-scheduled spacewalk to inspect the place, where Soyuz-TM17 hit the Mir- station. (probably near the APAS89 docking device on Kristall -Module-T).

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 January 24 - Mir News 205: Soyuz-TM18 flown from aft to forward docking port . 

    Mir-station:

    This operation was on schedule for 21.01.94 but was put back to 24.01.94. Instead of a short operation (undocking, hovering until the complex turned 180 degrees and docking to the other port) TsUP decided to use the operation for an inspection of the whole complex to be sure that the collision of S- TM18 and the Kristall-module on 14.01.94 did not cause fatal damages. The whole crew went aboard the Soyuz-TM18 and undocked from the aft docking port at 0309 UTC and flew autonomously for a long time. At 0452 UTC Soyuz-TM18 docked to the forward (P.Kh.O.) docking port and remained on board of the Soyuz-TM18 until 0619 UTC. During the first pass of the complex within our range (orb. 45359, 0615 UTC) Usachov reported via 121.750 mc that Afanasyev had opened the hatch. During the long period between docking and entering the station the crew checked systems and airseal of compartments.

    Damage assessment during inspection flight:

    Apart from some negligible scratches in the area of the collision (on Kristall-module) no significant or fatal damages have been discovered. In a long communication session between TsUP and Mir via Altair (0855-0946 UTC) the crew extensively reported about that inspection and transmitted images to earth. Obviously it will not be necessary to insert an unscheduled spacewalk to inspect the outer surface of Kristall.

    Progress-M21: This freighter will be launched from Baykonur on 28.01.94 at 0212 UTC. Docking 2 days later to Mir's aft (Kvant) docking port on 30.01.94 at abt. 0300 UTC.

    Yevpatoriya: The tracking and communication facilities near Yevpatoriya and Simferopol on the Crimea are again operational for TsUP's control of the Mir-space station. On 20.01.94 (orb. 45300, 1137 UTC) the crew waited for communications via Yevpatoriya. Meanwhile this has been confirmed: the RKA and her Ukrainian counterpart have reached an agreement on the use of Ukrainian space facilities for Russian spaceflight.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 January 28 - Progress M-21.  Spacecraft: Progress M. Mass: 7,130 kg (15,710 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 30 Jan 1994 03:56:13 GMT. Undocked on 23 Mar 1994 01:20:29 GMT. Destroyed in reentry on 23 Mar 1994 05:13:00 GMT. Total free-flight time 2.23 days. Total docked time 51.89 days.

  • 1994 January 29 - Mir News 206: Progress-M21 launched. 

    The freighter Progress-M21 was launched from Baykonur on 28.01.94 at 0213 UTC. Already at 0514 UTC the transmissions of Progress-M21 on 166, 165 and 922.755 mc could be heard. During the rest of Progress-M21's passes within our range the transmitters worked continuously. Progress-M21 will deliver supplies, food, water, fuel, equipment, spare parts and post to the Mir-complex. Progress-M21 does not carry a VBK (ballistic return capsule). This crew (the 15th Main Expedition) will receive another 2 Progress-M-s. The first one, the Progress-M22, will start on 16 (or: 18) March 1994. Progress-M22 will not carry a VBK. Progress-M23 is on schedule for launch on 18 (or: 20) May 1994 and will have a VBK on board.

    Expected docking time of Progress-M21 to Mir:

    On 30.01.94 at abt. 0354 UTC Progress-M21 will dock to Mir's aft (Kvant-1) docking port. The approach and docking will be automatically with the system Kurs. Afanasyev will be standby with the TORU (tele-orientation and command regime) which might enable him to take over manually in case of a Kurs system failure.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 January 31 - Mir News 207: Progress-M21 docked to the Mir-space station. 

    On 30.01.94 at 0356 UTC (03 hrs 56 mins 14 secs) the freighter Progress-M21 docked to the aft (Kvant) docking port of the Mir-complex. Afanasyev did not have to use the TORU for the Progress-M21 approached and docked automatically with the system Kurs. During the pass in orb. 45452 (0520 UTC) checks of the airseal proved that all was in good order and Afanasyev opened the hatch to the freighter at 0524 UTC. During the next passes the crew reported their satisfaction about the state of the Progress-M21: all was clean and fresh and the people on earth had taken good care for the cargo.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 February 11 - Mir News 208: Mir again can be montiored. 

    For a period of almost a fortnight Mir passed over here during the night hours and this meant radio silence on 143.625 mc. Now we again can monitor traffic during the evening hours. 145.550 mc remained active all the time, mainly with Packet radio. During the first passes this week the Mir crew spoke with their colleagues Manarov (U2Mir), Volkov (U4Mir) and Artsebarskiy (U7Mir) in Russia and Tognini in France. These contacts were in the Russian language and they used their operational call sign 'Derbenty'. The 145.550 mc was also in use on board of the space shuttle Discovery (STS-60) during the flight of the Russian 'astronaut' Krikolyov, who got permission for the temporary use of his own call sign U5Mir. The contacts between Discovery and Mir took place out of our range. On 8.02.94 they communicated via TDRS-es and the first direct contact on VHF took place on 10.02.94. During the night and early morning of 10.02.94 both objects regularly passed within our range during overlaps of their footprints.

    Schedule for operations with Progress-M freighters:

    Progress-M22: Launch on 16.03.94, docking with Mir on 18.03.- 94. This freighter does not carry a VBK (ballistic return capsule). Progress-M21: Separation from Mir on 17.03.94 if Progress-M22 is in the right orbit and functioning normally. Progress-M21 has no VBK on board. Progress-M23: Launch on 18.03.94, docking to Mir at 20.04.94. This freighter carries a VBK. Progress-M22: Separation from Mir on 19.05.94 if all is going well with Progress-M23. A schedule for the freighters after Progress-23 has been published, but data might be subject to changes. The transport ship Soyuz-TM19, had to be launched on 24.06.94, but this launch has been put forward to 20.06.94, docking to Mir on 22.06.94. The first crew consisted of Malenchenko, Musabayev and Strekalov. Strekalov had to return with the relieved Afanasyev and Usachov after 12 days. Possibly Strekalov will fly with Soyuz-TM21 together with Dezhurov and an American cosmonaut on 01.03.95.

    American 'cosmonauts': 2 American astronauts had to arrive in Starcity near Moscow on one of these days to begin with their training for a flight as 'cosmonaut'. Due to technical reasons their departure has been postponed for 1 or 2 weeks.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 March 15 - Mir News 209: Launch Progress-M22 postponed. 

    This freighter was on schedule to be launched on 16 or 18.03. Due to very bad weather conditions (blizzards) the launch has been put back for a while. Possibly the exact date of launch will be published on 17.03.94.

    Fire on Baykonur: On 7.03.94 a heavy fire broke out in a MIK (Assembly and test complex) and spread to a Maintenance Unit Headquarters. There the fire damaged a Telemetry installation. The fire caused a damage of appr. 1.7 a 1.8 million dollars. The Russians declared that space-programs will not suffer from this event.

    Progress-M17: This freighter has been flying autonomously from 11.08.93 for a duration test of its systems. The Russians planned to leave the Progress-M17 in orbit for a year and a half on request by the Americans who want to use modified versions of the Soyuz-TM-ships for ACRV (assured crew return vehicle) for the space station Alpha. A test flight with a Progress-M was useful for a lot of systems of this freighter are the same as those of the Soyuz-TM. During an orbit manoeuvre in December 1993 something went wrong and the Progress-M17 came in a very low perigee from where it decayed naturally by burning up in the Earth's atmosphere on 3.03.94 at 0406 UTC

    Tracking ships: The tracking ship Cosmonaut Pavel Belyayev is floating somewhere in the Atlantic for the support of spaceflight operations which have nothing to do with the Mir-station. Nevertheless the ship now and then assists TsUP for communications with the Mir-station. This took place on 13.03- .94 at 2004 UTC and on 14.03.94 at 2045 UTC, so out of our range. We can expect that within due time we can hear Mir- radio traffic relayed by the KPB or one of the other ships.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 March 22 - Progress M-22.  Spacecraft: Progress M. Mass: 7,103 kg (15,659 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Launched into an initial 192 x 238 x 51.6 km orbit. Docked with Mir on 24 Mar 1994 06:39:37 GMT. Fired its engine around 15 May to raise the orbit of the Mir station from 381 x 400 km to 398 x 399 km. Undocked on 23 May 1994 00:58:38 GMT. Destroyed in reentry on 23 May 1994 04:40:00 GMT. Total free-flight time 2.23 days. Total docked time 59.76 days.

  • 1994 March 23 - Mir News 210: Progress-M22. 

    This freighter will be launched from Baykonur on 22.03.94 at 0454 UTC for a flight to the Mir-space station. This launch, originally planned for 16 or 18.03.94, has been postponed due to problems on Baykonur. Russians sources stated that meteorological conditions (blizzards) had forced them to put back the launch. On 7.03.94 a heavy fire broke out in the MIK (assembly- and test complex) for Progress-M-s and Soyuz-TM- s. The fire also effected a command centre. It was almost impossible to extinguish this fire due to the lack of water caused by one of those inclement blizzards.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 March 25 - Mir News 211: Progress-M22 launched. 

    The freighter Progress-M22 has been launched from Baykonur on 22.03- .94 at 0454 UTC. If all goes well the Progress-M22 will dock to Mir's aft (Kvant-1) docking port on 24.03.94 at abt. 0638 UTC. During some of the passes within our range the transmitters of Progress-M22 could be heard. During the pass from 0929-0931 UTC only in the 166 and 165 mc bands, from 1059-1105 UTC also the beacon on 922.755 mc transmitted. So the transmitters did not -as usual- transmit during all passes. TsUP stated that all systems worked without problems. TsUP emphasised that the delay of the launch (originally on schedule for 16 or 18.03.94) was caused by the blizzards and that the fire in MIK and a command centre on 7.03.94 had nothing to do with the delay. The blizzards buried the cosmodrome under snow dunes up to 6 meters high.

    Tracking ships: Now and then TsUP and Mir meet problems with the communications via the geostationary satellite Altair. Probably this is caused by malfunctions of the meanwhile worn out transceiver (Antares) on board Mir The tracking ship Cosmonaut Pavel Belyayev (KPB), somewhere in the Atlantic, regularly is involved in Mir-communications. On 23.03.94 from 1705-1714 UTC Mir and TsUP have a communication sched via KPB.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 March 26 - Mir News 212: Progress-M21 separated from the Mir-space station. 

    As of 30.01.94 this freighter occupied the aft (Kvant-1) docking port of the complex. To enable the new freighter, Progress-M22, to dock to that port Progress-M21 had to disappear. On 23.03.94 at 0118 UTC Progress-M21 undocked and flew its last flight as an independent satellite until 0432 UTC. At 0432 UTC Progress-M21's engine gave an impulse to bring her back in the atmosphere. Consequently she burnt up and decayed over the Pacific a few minutes later. Progress-M21 had no ballistic return capsule on board.

    Progress-M22 docked to the Mir-space station:

    Progress-M22 docked to the aft (Kvant-1) docking port of the complex on 24.03.94 at 0639 UTC. The docking took place just after LOS of Mir and Progress-M22 for my position. During the pass before the docking Mir's radio traffic on 143.625mc and Progress-M22's beacon on 922.755mc could be heard. Afanasyev reported data about the approach: the final approach, distance 59 M, approach speed 0.3M/sec, etc. Already during the next pass (orb. 46281, 0803 UTC) the hatch to Progress-M22 had been opened. Inside Progress-M22 all was clean and the crew -as always- enjoyed the nice smell of apples. Progress-M22 delivered to the complex food, water, fuel, post, spare parts and equipment for the maintenance of Mir's systems and additional equipment to be used by Dr. Polyakov for his medical experiments. If the Russians stick to the original schedule Progress-M22 will have to leave the aft docking port on 19.05.94 to enable her successor Progress-M23 to dock on 20.05.94. Progress-M22 does not have a VBK on board; Progress-M23 will carry a VBK.

    Baykonur: As of 22.03.94 Russian and Kazakhstan politicians and experts are gathered in Moscow for negotiations on a draft agreement about the right of Russia to use the cosmodrome Baykonur. Thus far it was impossible to reach consonance about the amount of money for the rent and the compensation for ecological damages caused by soviet space-activities over some decades. Russians are considering the possibility to reconstruct the base for ICBM's near Svobodnyy (East Siberiya, 51degr24min N, 128degr07min E.) into a cosmodrome to replace Baykonur. Yuriy Semyonov, Head of NPO 'Energiya', is against this idea: in his opinion Russia will loose its place as a leading space-power if Russia abandons Baykonur. Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 May 10 - Mir News 213: Mir-operations. 

    After the docking of Progress-M22 to the Mir-station the passes gradually shifted to the night hours. Meanwhile Mir passes take place again during the day hours, which means that regularly radio traffic can be heard. In this stage of the Mir- mission there is not too much to report: just routine matters and the well-known experiments: measurements of the flows of elementary charged particles by the Mariya-spectrometer and x- ray and gamma radiation by spectrometers in the Kvant-1 module. The crew shot a lot of video- and photo-images of the earth on request by geologists en ecologists. Polyakov continues his medical experiments. On 9.05.94 the crew made films of heavy fires along the frontier of Siberia and Mongolia. During passes in which Mir is in contact with TsUP often only Afanasyev is heard. Sometimes, but not as much as Afanasyev, Polyakov and Usachov communicate with TsUP. Daily routine for the crew still remains the functioning of the water regeneration systems, about the SRV-U -distillation of water from urine- they daily have discussions with TsUP.

    Baykonur: After long and difficult negotiations Russia and Kazakhstan reached an agreement about the use by Russia of Baykonur and Leninsk. Russia has to pay a rent of 115 million. US-dollars a year for a period of 20 years and the option for a prolongation by another 10 years. Russia can act in Baykonur and Leninsk as if it was Russian territory. Let us hope that the agreement puts an end to the uncertainties for Russian and future users of the cosmodrome and to the vexations and confiscation of vital materials by the Kazakhstan authorities.

    Soyuz-TM19: This transport ship will be launched from Baykonur on 24.06.94 with the crew for the 16th Main Expedition to Mir. The first crew consists of Musabayev and Malenchenko, both rookies. Musabayev is from Kazakhstan, but the Russians stressed that he will fly just because he is a good cosmonaut and not to please Kazakhstan. On 4.04.94 the State commission decided to exclude Strekalov from that flight. He was on schedule for the Russians use to add an experienced cosmonaut to a crew with only rookies. So for the first time in many years a Soyuz-ship will fly with only rookies on board. The reason for the exclusion of Strekalov is economical: his seat will be used for an extra amount of cargo (85 KG). Strekalov is still in the race for he will fly during the 1995 program. He will then be 'ferried' to Mir by the space shuttle Atlantis. To get the training as an 'astronaut' he will arrive in the USA one of these days.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 May 17 - Mir News 214: Mir-operations. 

    On 16.05.94 the engines of the Progress-M22, still docked to the Mir-space station, corrected the orbit of the complex. The orbit on appr. 400 KM is almost fully circular now. Kepler elements earlier than 16.05.94 cannot be used any longer. Herewith the 2-line elements for day 137: 137.63180416 0.00005592 51.6463 339.1528 .0001314 282.2347 77.8458 15.56018306 47128. Progress-M23: The launch of this freighter has been put back until 22.05.94 at abt. 0425 UTC. If all will go according to plan we can for the first time monitor the transmissions of Progress-M23 that day at abt. 0725 UTC on the freq.-s 922.755, 166.140, 166.130 and 165.873 mc. Progress-M23 will have a VBK (ballistic return capsule) on board.

    The docking of Progress-M23 to the Mir-complex is scheduled for 24.05.94 at abt. 0617 UTC, so 4 minutes after LOS (Loss of signal) for our position.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 May 22 - Progress M-23.  Spacecraft: Progress M. Mass: 7,117 kg (15,690 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir, with Raduga return capsule. Docked with Mir on 24 May 1994 06:18:35 GMT. Undocked on 2 Jul 1994 08:46:49 GMT. The braking engine was ignited at 14:44 GMT, and the Raduga VBK reentry capsule was ejected at 14:55:45 GMT. The Progress burnt up in the atmosphere at 14:57 GMT. The Raduga deployed its parachute after reentry and landed on 2 Jul 1994 15:09:00 GMT at 51 deg 41 min N, 59 deg 21 min E, in the Orenburg region. Total free-flight time 2.34 days. Total docked time 39.10 days.

  • 1994 May 25 - Mir News 215: Progress-M23. 

    This freighter has been launched from Baykonur on 22.05.94 at 0430 UTC. During the first pass for our position the transmitters of Progress-M23 did not work possibly due to the fact that Yevpatoria still does not participate in the tracking activities of TsUP. During orbit 4 the transmissions on 166, 165 and 922mc could be monitored over here. Progress-M23 carries more than 2000 KG cargo for the Mir- complex, i.e. fuel, food, water, post, equipment and experiments. In contradiction to her predecessor this Progress-M also carries a VBK (ballistic return capsule).

    Progress-M22: This freighter had to free the aft (Kvant-1) docking port for the Progress-M23. After TsUP was sure about the good functioning of all systems of Progress-M23 Progress-M22 could be separated from Mir for decay in the atmosphere. The undocking took place on 23.05.94 at 0057 UTC and after some hours Progress-M22 burnt up over the Pacific.

    Progress-M23 docked to the Mir-station on 24.05.94 at 0619 UTC. During the first pass, in which the approach of Progress-M23 to Mir was in its final stage, there was no radio traffic on VHF (possibly again due to the absence of the Yevpatoriya- facilities). For communications TsUP used the Ku-bands of the Altair satellite. During the 2d pass (orb. 47232, 0745-0751- UTC) Polyakov reported from Mir's central post that Afanasyev and Usachov already were near the opened hatch to the Progress-M23. They had followed the safety recommendations of TsUP (for instance the use of protection glasses). The Progress-M23 was clean and already had given the whole complex a higher pressure to 717mm. The crew enjoyed the fresh air with the smell of fruits. Afanasyev reported that all was well. Launch date Soyuz-TM19 possibly put back:

    There are circulating messages about a possible change of the launch date of Soyuz-TM19, thus far on schedule for 24.06.94. These messages are not equal: there might be a delay until 20.07.94, but the Russians did not confirm this. They admitted that there are discussions about a possible delay, but if so the launch will take place not mare than 2 weeks later. The discussions are still going on.

    Yevpatoriya: For a short period in the beginning of 1994 this station could be used by the Russians for TsUP- Mir communications. During the flight of the Soyuz-TM18 the station could be used due to a provisional agreement between the RKA and her Ukrainian counterpart. Regretfully this probably only worked for a short period. Tough negotiations between Russia and the Ukraine were going on about this matter and the present problems on the Crimea certainly will not make the negotiations easier. Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 June 25 - Mir News 216: Soyuz-TM19. 

    The launch of this ship had been put back several times due to problems with the production of the fairing for the protection of Soyuz-TM19 during the first phase of the launch. Now this launch from Baykonur is on schedule for 1.07.94 at abt. 1224 UTC. If all goes well Soyuz-TM19 will dock to the Mir- complex (aft, Kvant-2 docking port) 2 days later. This ship will ferry the relief crew, Malenchenko and Musabayev, to Mir. On 9.07.94 the present crew Afanasyev and Usachov will return to earth with the Soyuz-TM18. Dr. Polyakov will remain on board to reach a place in the Guiness Book of Records after a stay of 429 days in space.

    Kazakhstan insists upon the fact that Musabayev will make his spaceflight as a representative of Kazakhstan for he is a native of that country. The Russians agreed with that, but told Kazakhstan that this means that Musabayev will fly as a foreign guest cosmonaut and that Kazakhstan has to pay for that just like western countries have to pay for their cosmonauts. Kazakhstan cannot afford this.

    Progress-M23: Before Soyuz-TM19 can dock to the aft docking port the freighter Progress-M23 has to undock from there. If all goes well on board Soyuz-TM19 after launch Progress-M23 will separate from Mir on 2.07.94. The return capsule (VBK) of Progress-M23 has to make a soft landing somewhere in Kazakhstan.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 July 1 - Soyuz TM-19.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-16. Soyuz TM-19 docked at the rear port of the Kvant module (vacated by Progress M-23 on July 2) at 13:55:01 GMT on July 3.

  • 1994 July 1 - Mir News 217: Soyuz-TM19 launched for flight to Mir. 

    Soyuz-TM19 started from Baykonur on 1.07.94 at 1224 UTC.

    Soyuz-TM19 has a crew of two: Yuriy Malenchenko and Tolgat Musabayev. For a long time the status of this flight was unknown: Musabayev's native country is Kazakhstan, but he was supposed to fly as an officer of the Russian airforce. Now the flight has been announced as a Russian-Kazakh expedition. Russia paid for the preparations and Kazakhstan will pay a contribution for Musabayev's activities on board Mir. All went well during the launch and the first day of the flight. The cosmonauts use the call sign Agat-1 and Agat-2. The crew has no problems with micro-gravity and space sickness. During the 3d orbit at 1527 UTC the ship came in our range. Malenchenko reported that all was going according to plan and the results were positive. The pressure of the atmosphere on board was 803 mm. Already during the next pass (orb. 4, 1656 UTC) Malenchenko reported the first 2 orbit corrections accomplished as needed and without any problems. During the following pass (orb. 5, 1837 UTC) Malenchenko announced that the 3d orbit correction would take place at 18 hrs 47mins and 45 secs UTC. As usual during such flights: radio contact with TsUP on 121.- 750 mc and telemetry and beacons on 166, 165 and 922.755 mc.

    Progress-M23: As soon as TsUP was sure that all went well with Soyuz-TM19 the undocking of Progress-M23 was possible and took place on 2.07.94 at 0841 UTC. The landing of the VBK (ballistic return capsule) had to take place on 2.07.94 at 1500 UTC at 150 KM North East of the town Orsk, within Russian territory, so no need to pay import duties.

    Estimated docking day and time of Soyuz-TM19 with Mir:

    3.07.94 at 1404 UTC, so just after LOS for us after the first pass of Mir and Soyuz-TM19 for our position.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 July 3 - Mir News 218: Soyuz-TM19 docked to Mir-space station. 

    Soyuz-TM19 docked to the aft docking port (Kvant-1) on 3.07.94 at 1355 UTC, so 9 minutes earlier than planned. Approach and docking took place in the automatic mode by the system Kurs. So during the pass in orb. 47859, 1355-1402 UTC, the docking just took place. By monitoring Altair OM Peter could determine the right docking time meanwhile confirmed by TsUP. During the 2d pass (orb. 47860, 1527 UTC) the crew for the 16th Main expedition already had joined their predecessors inside Mir itself. During radio contact with the tracking ship Kosmonavt Pavel Belyayev in the 3rd pass (orb. 47861, 1704 UTC) Talgat Musabayev told that he was very pleased to be on board and that he did not suffer from adaptation problems at all. He also stated that he does not have any problems with the status of this flight: Russian, Russian-Kazakh, CIS or international. He considers himself to be a representative of all human beings on earth. He also emphasised that nothing can hamper the good friendship between the Russian an Kazakh people (let us hope this also applies to the politicians!).

    16th Main expedition to Mir:

    This mission consists of the new crew together with Doctor Polyakov. Malenchenko and Musabayev will return to earth on 2.11.94. Together with the new enthusiastic cosmonauts Soyuz-TM19 delivered to Mir hard- and software for experiments during the Euromir 94 mission of Merbold in October this year. In September 1994 Mal. and Mus. have to make 4 EVA (spacewalks) aimed at the transfer of the solar panels from Kristall to Kvant-1, maintenance and inspections of the outer surface of the complex and the replacement of containers (among other things the American Trek-experiment) with experiments exposed to open space.

    Soyuz-TM18: The relieved crew (Afanasyev and Usachov) will return to earth by this ship on 9.07.94.

    Progress-M23: This freighter undocked from Mir on 2.07.94 at 0841 UTC and decayed in the earth's atmosphere the same day. Just before decay it jettisoned the VBK (ballistic return capsule) which made a safe landing within Russian territory 150 KM N.E. of the town Orsk at 1508 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 July 9 - Mir News 219: Soyuz-TM18 safely landed in Kazakhstan.. 

    The relieved cosmonauts Afanasyev and Usachov landed with the Descent Module of the Soyuz-TM18 at 100 KM NE of Arkalyk on 9.07.- 94 at 1033 UTC. Radio traffic of Soyuz-TM18 during the descent -also the ANAN aiming beacon- could be monitored via Altair until 1020 UTC. Immediately after the landing the cosmonauts boarded an aircraft for a non-stop flight to Star City near Moscow.

    Mir: 2 days ago the command of the Mir-complex was handed over by Afanasyev to Malenchenko. From this moment on the call sign of Polyakov changed from Derbent-3 to Agat-3.

    Soyuz-TM19: This ship is still docked to the aft (Kvant-1) docking port of the Mir-complex. Contrary to the normal practice this ship will remain there, so no redocking from the aft to the forward docking port has been planned. One of the reasons may be the future operations with modules like Module- T (Kristall), Spektr and Priroda.

    Progress-M24: Thus far the launch of this freighter is still on schedule for 13.07.94.

    Tracking ships: On 8.07.94 the tracking ship Kosmonavt Pavel Belyayev moored in the port of Antwerp. A few hours later I visited the ship for a long interview with the Chief of the Expedition of KPB. I was able to follow the movements of the ship and to determine her destination by monitoring radio traffic between the ship and the Mir-station. The chief answered a lot of questions regarding the fate and future of the famous fleet of tracking ships. The KPB is now on her way to Sankt Peterburg. A ship to take over her task in the Atlantic did not show up but remained in Sankt Peterburg due to budget problems.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 July 9 - Landing of Soyuz TM-18. 

    Soyuz TM-18 landed at 10:32 GMT, 110 km north of Arkalyk in Kazakhstan, with the crew of Afanasyev and Usachyov aboard.

  • 1994 July 17 - Mir News 220: Progress-M24. 

    The launch of this freighter has been put back. Originally 2 Progress-M's had to be launched in the period July/August 1994. The Russians had to give up one of the Progress-Ms for economical reasons. Now the Progress-M24 is on schedule to be launched on 24.08.94. Progress-M24 will deliver the normal cargo to the Mir-complex plus the equipment to be used by an European cosmonaut (Ulf Merbold or Pedro Duque) during the EuroMir94 mission in October 1994.

    Soyuz-TM19: This ship is still docked to the aft (Kvant-1) port of the Mir-station. Contrary to the normal practice S- TM19 will not be redocked to the forward (PKhO) docking port of the complex.

    EuroMir94: The Soyuz-TM20 with on board the relief crew (Viktorenko and Kondakova or the stand-in crew Gidzhenko and Avdeyev) with an ESA-cosmonaut (Ulf Merbold or Pedro Duque) is on schedule for launch on 3.10.94. The European cosmonaut will remain on board Mir for a period of 30 days. The training of the crews takes place in Starcity near Moscow as well as in the European Astronaut Centre of ESA in Cologne. In Moscow they have to study the Russian language and to get familiar with the Soyuz-TM and the Mir-space station and its modules and in Cologne the training is aimed at the European experiments, which for the greater part will cover life-sciences, i.e. monitoring the human body in microgravity conditions.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 July 25 - Mir News 221: Russian spaceflight tracking ships.. 

    Until 1992 the fleet of tracking ships consisted of ten ships. These ships formed a part of the infrastructure of control centres and measurement points for soviet spaceflight operations. In this case the word 'operations' covers a wide variety for the assistance of the manned spaceflight program was only a small part of their duties. The role of the ships, as far as manned spaceflight was concerned, sharply deteriorated after the beginning of the use of geostationary satellites for communications between the Salyut-7 and the Mir-space stations. The TDRS system used by the Russians did not always work satisfactorily and so all experts involved in Russian spaceflight expected that the 'ships' would remain operational at least until 2000. Already in 1990 there circulated rumours about the a gradual withdrawal of that fleet, but nobody dared to take the responsibility. However the economical problems in the last year of the S.U. forced the Russians to withdraw most of the ships from service and as of January 1st 1992 the ships in the Atlantic apart from some modest exceptions ceased to assist during Mir-operations. Sometimes a ship was operational in the Atlantic to assist space-operations for other objects and organisations and now and then had to be stand-by during Mir-operations (launches of Progresses, Soyuzes, dockings, return operations, EVA's a.s.o.), but always on a secondary basis. For the last half year the Kosmonavt Pavel Belyayev operated from a position west of Africa and even played an important role during the almost fatal flight of Soyuz-TM17 on 14.01.94. After some bumps of the Soyuz-TM17 into the Mir-station the communications via the Altair (Cosmos-2054) ceased and this caused great concern at TsUP. KPB was the first to pick up radio traffic from the Soyuz-TM17 and thus shortened the awful uncertainty phase at TsUP by 10 minutes. In the past the ships relayed traffic between Mir and TsUP via Molniya satellites during the first part of Mir's footprint for our position. Nowadays the traffic between Mir and TsUP only begins at TCA for our position. The fate of the fleet: the ships belonged to the Soviet (now Russian) Academy of Sciences. The maritime part fell under the responsibility of the Baltic- and Black sea shipping. The ships which have home ports in the Ukraine (the Kosmonavt Yuriy Gagarin and the Akademik Sergey Korolyov) now belong to that country and so their role in spaceflight fully ceased. The ships made some trips for tourists, but that was not successful. Both ships have been used to evacuate Russian military personnel and their families from Cuba to St. Petersburg. From there they returned to their Ukrainian ports. The Ukraine does not know what to do with the ships and tried to sell them to the Russians. The Russians were not interested: they still have 4 ships for the Western Hemisphere and a 5th one is under construction. Spaceflight needs over the Pacific are covered by 2 ships of the Russian Navy, the Marshal Nedelin and the Marshal Krylov. The Odessa based Kosmonavt Vladimir Komarov already before the independence of the Ukraine was transferred to Leningrad to be refurbished for other purposes: ecological expeditions in the Baltic and the North Atlantic. Thus far this plan did not work: the attempts to use the ship for that purposes on a commercial base did not have success due to the lack of customers. So in St Petersburg we have 4 ships: the Kosmonavt Pavel Belyayev, the Kosmonavt Vladislav Volkov, the Kosmonavt Viktor Patsayev and the Kosmonavt Georgiy Dobrovolskiy. They are waiting for an assignment. Possibly one of them will be used in the Atlantic west of Africa in October and November 1994 to assist during the launch and docking of Soyuz-TM20 (resp. 3 and 5.10.94) and the return flight of the Soyuz-TM19 on 3.11.94. A new ship, the Akademik Nikolay Pilyugin, has already been launched and has to be fitted. Thus far it is not known whether this new ship will influence the fate of 1 or more ships of the 4 in St Peterburg. After the last expedition the Belyayev several times had contact with the crew of the Mir-complex. From this traffic I could derive the indication that the ship planned to visit Antwerp in Belgium. This enabled me to go on board and I had a long and interesting conversation with the chief of the expedition, Nikolay Burov and the captain Sivtsov. In spite of the enormous economical difficulties of their country their hospitality towards me was 100%.

    (This Mir-report is derived from the reports in Dutch 221 and 222. So the next Mir-report in English will be MirNEWS.223)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 July 30 - Mir News 222: Radio-amateur information. 

    Info for Radio-amateurs trying to make QSO's with Mir:

    On 30 July 1994 during pass in orbit nr. 48273 Musabayev asked TsUp to inform Sergey Samburov that the power unit of the transceiver for Radio-amateurism is out of order. The last time I monitored traffic on 145.550 Mc from Mir was on 27 July 1994 during the passes in orbits 48226 and 48227 when Polyakov (U3Mir) tried to make a QSO with Francis in France and with OE1AKB.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 August 16 - Mir News 223: Mir-operations. 

    These days Mir's passes for our position take place during the night-hours. During the Perseid meteorite streams no nightly radio-traffic on VHF, so obviously nothing happened. This in contradiction to the same period in 1993 when several particles collided with the Mir-station. In a few days we can expect radio traffic during the evening hours again.

    PROGRESS-M24: This freighter will be launched from Baykonur on 25.08.94 at 1425 UTC. If all goes according to the plan listeners in Western-Europe can receive radio signals on the known frequencies (166.140, 166.130, 165.874 and 922.755 + or - for Doppler) 3 hours later.

    Spacewalks (EVA-s): Instead of 4 only 2 EVA's will be made by Malenchenko and Musabayev. These EVA-s are scheduled for 8 and 12.09.94. Purpose: transfer of solar panels from Kristall to Kvant-1.

    SPEKTR: The launch of this Module-O has been put back again. Now there is word that the launch will take place in may 1995. Undoubtedly this will also mean that the launch of Priroda (Module-E) will be put back either.

    American flights to Mir: The schedule for these flights might be changed due to the delay of the launch of Spektr. No further details yet.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 August 25 - Progress M-24.  Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Failed to dock with Mir on 27 Aug 1994. A second automatic docking attempt on 30 Aug 1994 also failed and the Progress collided with the Kvant module. A third and final attempt, manually controlled by Mir commander Yuriy Malenchenko, was successful on 2 Sep 1994 13:30:28 GMT. The Mir commander and flight engineer, Yuriy Malenchenko and Talgat Musabaev, made a spacewalk on 9 Sep 1994 to inspect the damage to the Kvant module made when the Progress collided with Kvant. Undocked on 4 Oct 1994 18:55:52 GMT, leaving the rear docking port free for Soyuz TM-20. Destroyed in reentry over the Pacific at 38.4 deg S, 137.4 deg W,on 4 Oct 1994 22:43:00 GMT. Total free-flight time 8.12 days. Total docked time 32.23 days.

  • 1994 August 25 - Mir News 224: Progress-M24. 

    A Soyuz carrier with the freighter Progress-M24 blasted off from Baykonur on 25.08.94 at 1425 UTC. The Progress-M24 has to deliver to the Mir-space station food, water, fuel, post for the crew, spare parts and equipment for repairs, also for the radio-amateur installation, and experiments to be used during the Euromir94 expedition in October this year. The Progress-M24 does NOT carry a VBK (ballistic return capsule). The telemetry- and beacon transmitters in the 166, 165 and 922 Mc bands could be monitored here during the passes in the 2d, 3d and 4th orbit. The estimated docking time with Mir is on 27.08.94 at 1601 UTC, so appr. 5 minutes after LOS of Mir's pass in orbit 48715. Progress-M24 will have to dock at the forward (PKhO) docking port.

    Recently the cosmonauts checked the system TORU (teleorientation and guidance) obviously to be ready to guide Progress-M24 manually from Mir during the approach and docking if necessary.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 August 27 - Mir News 225: Progress-M24. 

    During the preparations for the docking of this freighter to the Mir-complex something seemed to be wrong with some systems of that ship. TsUP decided to discontinue the approach-procedure and to maintain Progress-M24 in an autonomous status for the time being. A commission is investigating the causes of the problem and must to decide when a second docking attempt will be made. Probably this will last 3 or more days.

    Radio traffic: The fact that there might be something wrong could be derived from TV-images received via Altair by our good friend Peter and from the radio traffic thereafter. In the period in which the 'final approach' was planned the crew changed the orientation of the Mir-complex to get better visual observations of the 'naughty' Progress-M24. The transmitters of the Progress-M24 in the 922, 166 and 165 Mc bands transmitted continuously. During the 2d pass of the Mir-station (orb. 48716, 1725-1735 UTC) Progress-M24 still flew autonomously and from the radio traffic between Mir and TsUP could be derived that the cosmonauts tried to observe Progress-M24 visually. Progress-M24 flew a few kilometres (2.7 a 1.5) ahead of Mir on the same altitude. Visual observations: In those part of the Netherlands and UK where the sky was clear Mir and Progress-M24 could be seen flying separately from each other during Mir's orb. nr. 48718, 2038- 2046 UTC. The 'small' star Progress-M24 flew 6 seconds ahead of the 'huge' star Mir. TCA Progress-M24: 204051 UTC, TCA Mir: 204057 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 August 31 - Mir News 226: Progress-M24. 

    The 2d attempt to dock this freighter to Mir also did fail. The estimated docking time was 30.08.94 at 1450 UTC. The Progress-M24 softly hit the Mir-complex twice after which Progress-M24 immediately moved away. The Mir-crew felt the little shocks caused by the 2 contacts. They reported this during the pass in Mir's orbit 48762 at 1615 UTC. They also tried to assess eventual damages by looking through portholes. The transmitters of Progress-M24 functioned normally after the event.

    TsUP: In this flight control centre specialists did (until deadline of this report) not know the causes of both failures. More docking attempts are under consideration, but the decision depends on further analyses and results of meetings of specialists today. An eventual 3d attempt will not be made today (31.08). Among the possibilities is the use of the system TORU (Tele-orientation and guidance), which enables the crew to guide Progress-M24 from inside Mir.

    Consequences: These can be far-reaching for Russian manned spaceflight if further attempts to dock Progress-M24 would fail. Except from the normal cargo (food, water, fuel, repair material, post etc.) Progress-M24 had to deliver a part of the experiments for the Euromir94 mission and American equipment to enhance some systems on board Mir. The spare stock now available for life on board of the complex is enough for 1 month. So new supply before the end of September is urgently needed. Further failures can hamper the plans for the near future, i.e. the EVA-s in September, Euromir94 and the flights of American astronauts and Mir-Shuttle operation.

    (Derived from an enormous amount of information available until 31.08.94 at 1130 UTC.)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 September 2 - Mir News 227: Progress M-24 docks to Mir.. 

    TO BE ALLOWED TO TRY THREE TIMES RUNNING IS BUT FAIR!!

    The 3d attempt to dock the freighter Progress-M24 to Mir succeeded. This time they used the system TORU instead of Kurs. Malenchenko safely guided and docked Progress-M24 to the forward axial docking port (P.Kh.O.-transition section). The docking took place on 2.09.94 at 1330 UTC. During the last phase of the approach Malenchenko was fully responsible and in an admirable way he performed his task. Molodets!! Voice communication between Mir and TsUP via Altair was loud and clear and so I was able to monitor the actions and observations of Malenchenko. Just before docking the voice communication stopped while Progress-M24 was on a distance of 5 Meters with an approach speed of 26 cm/sec. M. had to correct Progress-M24's course due to a slight deviation to left.

    Radio traffic via VHF after the docking:

    During the pass in orb. 48809 (1648 UTC) M. reported that the hatch had been opened and that they already more or less had started the unloading. The ship was in good order and all was clean. The crew had to unload the container Biokrist and install it in the right place as soon as possible. (Biokrist is complex of protein crystallisation experiments) During the next pass (orb. 48810, 1824 UTC) the main subject again was the cargo and the special attention for the container Biokrist).

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 September 6 - Mir News 228: Spacewalks (EVA's). 

    The delay in the arrival of the freighter Progress-M24 will not cause significant changes in the original programme for the near future. The EVA's to be made in September have been put back by only 1 day: so to 9 and 13.09.94. The EVA on 9.09 will start at abt. 1300 UTC. The schedule for 13.09 depends on the results of the 1st EVA. The main task during these EVA's will be the transfer of the solar batteries from Module-T (Kristall) to Module-E (Kvant-1).

    Euromir94:

    Rumours suggested a substantial delay of the beginning of that mission. This has not officially been confirmed. Officially has been stated that it might be possible that Soyuz-TM20 with the European cosmonaut on board will blast off on 4.10.94, so 1 day later.

    Chris van den Berg, NL-9165/A-UK3202.

  • 1994 September 9 - EVA Mir EO-16-1.  Spacecraft: Mir.

    Repaired station external insulation. Checked docking port.

  • 1994 September 13 - EVA Mir EO-16-2.  Spacecraft: Mir.

    Checked out equipment on exterior of Mir.

  • 1994 September 13 - Mir News 229: 2 Spacewalks (EVA-s). 

    On 9.09.1994 Malenchenko and Musabayev worked in open space for the first time. The duration of the EVA was more than 4 hours (a reliable source even spoke about 5 hrs 2 mins.). During the pass in orb. 48915, 1200-1207 UTC, so within our VHF-range, they reported the closure of the hatch at 1202 UTC. During this EVA they inspected the outside of the whole complex, installed on outside platforms experimental materials for exposure to open space and removed other experiments of that kind for storage inside the complex. They repaired the damaged thermo-isolation layer on the transition section (P.Kh.O.) of which a piece of 30x40 cm had been torn away during the collision with Soyuz-TM17 in January 1994. The inspection made clear that the touches of the freighter Progress-M24 during its 2d approach on 30.08.94 did not cause significant damages.

    On 13.09.1994 they worked in open space for the 2d time. The EVA lasted 6 hrs and 1 min between 0631 UTC (opening of the hatch) and 1232 UTC (closure of the hatch). The cosmonauts did a lot of minor repairs, replacements of bolts, screws, etc. of platforms and equipment on the outer surface of the complex. They also spoke about an old antenna. Activities of that kind must be done now and then, but have been often neglected during EVA's due to more important matters. The cosmonauts also did some preparatory work aimed at the future transfer of the solar batteries from Kristall to Kvant-1. This transfer has been put back again, now even to the beginning of 1995.

    Radio communications: During EVA-s the frequency of the VHF- downlink is somewhat lower: 143.622 mc, shifting by Doppler to 143.617 mc. Listeners in Western-Europe, inclusive UK, who monitor Mir-traffic during EVA's often experience heavy interference caused by cross-modulation from an air traffic control frequency.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 September 29 - Mir News 230: Soyuz-TM20. 

    The preparations for the launch of this ship with the relief crew and the Euromir94 astronaut are proceeding normally. The launch from Baykonur is scheduled for 3.10.94 at 2242 UTC (so for Moscow: 4.10.94 at 0142 Msc Winter Time.) If all goes well during the 2-days flight the Soyuz-TM20 will dock to the Mir complex on 6.10.94 at 0013 UTC. Radio traffic and beacon signals from Soyuz-TM20 can be monitored in our area for the first time on 4.10.94 at abt. 0142 UTC on the known frequencies. The crews on the roll are still: Aleksandr Viktorenko (commander), Yelena Kondakova (board-engineer) and the ESA astronaut, the German Ulf Merbold. The stand-ins: Yuriy Gidzenko (comm.), Sergey Avdeyev (B.E.), and the ESA astronaut, the Spaniard Pedro Duque. If the state commission decides to appoint the main-crew for the flight the crew of Soyuz-TM20 will use the call sign Vityaz (so Vityaz-1, 2 and 3.)

    Mir: The Mir-crew is preparing the station for the extension of the crew with another 3 persons. Therefore the life-support systems get special attention. The crew also modified the ASU (waste collection equipment) for the use by a lady. The crew is also busy with the loading of the freighter Progress-M24 with garbage and no things which are no longer needed. The Progress-M24 will have to leave the complex to free the docking port for the Soyuz-TM20. There have been plans to execute some test-approaches by the Progress-M24 after the undocking to try to unveil the causes of the malfunction of the Kurs system during the unsuccessful docking attempts on 26 and 30.08.94. After that operation the Progress-M24 will burn up in the atmosphere over a designated area in the Pacific ocean. Progress-M24 does not carry a VBK (ballistic return capsule).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 October 3 - Soyuz TM-20.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-17. Docked at the Mir forward port at 00:28 on 1994 October 6. The Mir crew of Viktorenko, Kondakova and Polyakov boarded Soyuz TM-20 on January 11, and undocked from Mir's front port at 09:00 GMT. The spacecraft withdrew to about two hundred metres from Mir and then redocked in a test of the automatic Kurs system, which had failed in Progress M-24's attempted docking. Redocking came at 09:25 GMT.

  • 1994 October 4 - Mir News 231: Soyuz-TM20 launched.. 

    The Soyuz-TM20 with on board the Euromir94 astronaut Merbold and the cosmonauts Viktorenko and Kondakova blasted off from Baykonur exactly on schedule on 3.10.94 at 2242 UTC (Moscow time 4.10.94 at 0142 UTC). During the passes in our range during the orbits 2, 3, 4 and 5 at resp. 0143, 0312, 0445 and 0625 UTC the Soyuz-TM20 could be monitored on the known frequencies. At 0320 UTC Viktorenko, prompted by Kondakova, reported the successful first 2 orbit corrections and the additional data. It was obvious that all on board was going well. Judging by the cheerful voice of Kondakova she must be in a good condition. Kondakova wants to stay in orbit for approx. 6 months.

    Estimated time of docking to Mir:

    Result of calculations estimate the docking time of Soyuz-TM20 to Mir on 6.10.94 at 0013 UTC, ESA (still) sticks to 0030 UTC. Soyuz-TM20 has to dock to the forward (P.Kh.O.) axial docking port of the Mir complex.

    Progress-M24: This freighter still occupies that docking port and has to get away before the arrival of Soyuz-TM20. It might be possible that after the separation the Russians will check the system Kurs of Progress-M24 during some dummy approaches as to reveal the causes of malfunctions during recent unsuccessful docking attempts. Progress-M24 does not carry a VBK (ballistic return capsule) and will burn up in the atmosphere over an area in the Pacific.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 October 6 - Mir News 232: Soyuz-TM20 docked at the Mir complex. 

    Soyuz-TM20 docked at the Mir complex on 6.10.94 at 0028 UTC.

    Soyuz-TM20 docked at the forward axial docking port (transition section) of the complex. At a distance of 130 M. from the Mir complex Viktorenko had to take over manually due to a malfunction of an on board computer. During the radio traffic in orb. 49328, 0005 UTC, V. reported the progress of the operation. The Soyuz-TM20 was in a distance of 151 M., approach speed of 3 cm/sec just before LOS at 001148 UTC. From a distance of appr. 50 M Viktorenko had started the final approach and his skill amazed the observers in the ESA/EAC facility in Cologne: very quickly, with only a few corrections, he accurately moored his ship. During the next pass in orb. 49329, 0143 UTC, the new crew already was in Mir's base block preparing a TV-session. One of the first persons to congratulate the crew, especially the Euromir94 astronaut Merbold, was the Dir. General of ESA, Luton. Everybody in Cologne was pleased with the excellent physical condition of the newcomers. During the pass in orb. 49330, 0317 UTC, the cheerful meeting of both crews could be heard. Again there was a TV-session also with Kondakova. During the next window in orb. 49331, 0449 UTC, Viktorenko reported that he did all what he had to do with his ship Soyuz-TM20. Progress-M24: This naughty freighter had to withdraw before the arrival of Soyuz-TM20. Progress-M24 separated from Mir on 5.10.-

    94 at 1853 UTC. Probably she flew some orbits autonomously before burning up in the atmosphere over an area in the Pacific. There have been no reports about extra manoeuvres with Progress-M24.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 October 13 - Mir News 233: Failure power supply on board Mir. 

    In the night from 11 to 12.10.94 the voltage of the power supply sharply decreased. This failure had been caused by the insufficient charging by solar batteries. All systems in the base block discontinued functioning. From this moment on it was impossible to control the attitude of the Mir-complex. It became impossible to aim the antenna for communications via the geostationary satellite. During this night a lot of radio traffic via 143.625 mc was monitored in which the problems were reported and discussed. Opinions of Russian specialists are not unanimous: the VKS (Russian space forces) spoke of a very complicated situation. Deputy Flight controller Blagov of TsUP blamed the age of the station, which is in orbit as of the beginning of 1986, while the PRO of TsUP sounded rather optimistic. He stated that the Euromir94 expedition will remain on schedule. In the night from 12 to 13 Oct. Viktorenko and Kondakova remained on duty to be able to act if necessary. Meanwhile a lot of electric energy had been loaded and specialists hope to be able to adjust the attitude of the complex in such a way that the solar arrays will function as efficient as possible and that communications via the relay satellite will be restored. The cosmonauts did not panic at all: Viktorenko and Kondakova even joked about the fact that the exchange rate of the dollar on board Mir remained stable, which could not be said about the voltages of their power supply systems.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 October 31 - Mir News 234: Soyuz-TM19. 

    This ship with on board the cosmonauts Malenchenko, Musabayev and Merbold will return to earth on 4.11.94. The return flight has been put back 1 day. The Russians had to extend the Euromir94 mission for an extra test flight with the Soyuz-TM19. The crew of Soyuz-TM19 will close the hatch behind them on 4.11.94 at 0450 UTC. The ship will undock from the Mir-complex at abt. 0700 UTC and if all goes according to the so called 'cyclogram' the landing in Kazakhstan will follow at 1118 UTC.

    The inserted test flight of Soyuz-TM19 will take place on 2.11.94. The ship will separate from at 1100 UTC and execute some approaches to check the automatic Kurs system.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 November 2 - Mir News 235: Soyuz-TM19. 

    On 2.11.94 from 1040-1116 UTC this ship made an autonomous flight to test the automatic approach system. The crew consisted of Malenchenko, Musabayev and Merbold. No anomalies have been reported thus far.

    Euromir94: In spite of power problems in the beginning of this mission all medical-biological experiments during which Ulf Merbold, the ESA-astronaut, was the main guinea-pig have been successfully concluded. Merbold is sure that the samples did not suffer damages from the period in which the refrigerator was switched off. The material-processing experiments had to be cancelled due to the malfunction of an oven. The materials for these experiments remain on board Mir and after the repair of that oven the Russian crew will do the experiments. Spare parts for that oven will be delivered to the complex by the next Progress-M freighter.

    Estimated landing time Soyuz-TM19:

    The landing has been put forward a little bit and is expected to take place on 4.11.94 at 1055 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 November 4 - Mir News 236: Soyuz-TM19 returned to earth.. 

    Soyuz-TM19 with on board the cosmonauts Malenchenko, Musabayev and Merbold landed at abt. 170 KM N.E. of Arkalyk in Kazakhstan on 4.11.94 at 1118 UTC. Soyuz-TM19 separated from Mir at 0729 UTC. For radio- and TV-communications the tracking stations Ulan-Ude, Ussuriysk, Kolpashevo and Petropavlovsk Kamchatka were used. From 1020 UTC, so 3 minutes before retrofire, Soyuz-TM-19's traffic was relayed via Mir and the geostationary Altair satellite to TsUP. Malenchenko gave information about the retrofire, the fuel consumption and the altitudes of his ship. At 1051 UTC Soyuz-TM19 jettisoned the life compartment and the service module. These compartments burnt up in the atmosphere. At 1054 UTC the descent module entered the dense layers of the atmosphere and a short period of radio silence began. The radio contact had to be resumed at about 1101 UTC, but obviously due to a failure the transmitters of Soyuz-TM19 remained silent. This caused anxiety among 'observers' and the people following the events in the centres in Moscow, Toulouse, Cologne and Noordwijk (Estec). The controllers at TsUP did not get any reaction on their calls. At 1119 UTC a representative of ESA, who was on board of a search- en rescue helicopter, reported that he saw the landed capsule. Gradually reports came in about the safe landing of the cosmonauts without any reference to their physical condition.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 November 4 - Landing of Soyuz TM-19. 

    Soyuz TM-19 undocked from Mir with the crew of Malenchenko, Merbold and Musabayev aboard at 07:29 GMT on November 4. The Soyuz instrument module (PAO, priborno-agregatniy otsek) fired its deorbit engine, and was jettisoned together with the orbital module (BO, bitovoy otsek) at 10:51 GMT, with entry interface for the descent module (SA, spuskaemiy apparat) at 10:54. It landed 170 km north-east of Arkalyk in Kazakhstan on 1994 November 4 at 11:18 GMT.

  • 1994 November 9 - Mir News 237: Progress-M25. 

    The launch of this freighter from Baykonur is on schedule for 11 November 1994 at 0721 UTC. If all goes according to plan Progress-M25 will dock to the Mir-complex in the morning of 13 November 1994.

    Chris v.d. Berg, NL-9165-A-UK3202

  • 1994 November 11 - Progress M-25.  Spacecraft: Progress M. Mass: 7,125 kg (15,707 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 13 Nov 1994 09:04:29 GMT. Undocked on 16 Feb 1995 13:03:00 GMT. Destroyed in reentry on 16 Feb 1995 16:45:00 GMT. Total free-flight time 2.23 days. Total docked time 95.17 days.

  • 1994 November 11 - Mir News 238: Progress-M25 launched for flight to Mir.. 

    The freighter Progress-M25 blasted off from Baykonur on 11.11.94 at 0721 UTC for a flight of 2 days to the Mir station. The transmitters of Progress-M25 could be heard here during the 3d and 4th orbit at resp. 1157 and 1326 UTC. If all goes according to plan Progress-M25 will arrive at Mir on 13.11.94 at abt 0902 UTC. Progress-M25 has to dock to the aft (Kvant- 1) docking port of the station. The approach system for this port has been checked during a short autonomous flight of Soyuz-TM19 on 3.11.94. No anomalies were found. If the system fails on 13.11 the cosmonauts are ready to guide Progress-M25 with the system TORU.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1994 November 13 - Mir News 239: Progress-M25 docked at Mir-space station.. 

    The freighter P-M25 docked at Mir's aft (Kvant-1) docking port on 13.11.94 at 0904 UTC (during orb. 49926). The approach and docking took place in the automatic mode by the system Kurs. On board Soyuz-TM20 Viktorenko was standby with the system TORU, but manual interference was not necessary. The operation could be monitored via Altair between 0822 and 0904 UTC. During the next pass (orb. 49927, 1027 UTC) the gentlemen on board left the honour to give the first post-docking report to Yelena Kondakova. Enthusiastically she reported the airseal, the opening of the hatch, the fact that Progress-M25 was clean and that they enjoyed the nice smell of apples and lemons. Polyakov said that the Progress-M25 was an ideal freighter.

    Progress-M25 delivered to the Mir-station new supplies of water, fuel, food, spare parts for repair (among which parts for the furnace to be used for the conclusion of the Euromir94 materials processing experiments) and post. Progress-M25 has not been equipped by a VBK (Ballistic Return Capsule).

    Jubilees: In the early morning of 18.11.94 Mir -that is to say the first part, the base block, launched on 19.02.1986- will make her 50000th orbit around the Earth. From that early beginning I tried to monitor as much as possible all passes within range. If I was a robot and had been able to monitor all passes this number would be 12500. But not being a robot I needed holidays etc. Nevertheless at a rough estimation I must have been monitoring Mir's radio traffic during 10000 passes. Homage to my poor ear-drums!

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1994 Late or Early 1995 - Buran 5 (cancelled).  Spacecraft: Buran.

    Buran Flight 5 (3K1) would have been the first flight of the third orbiter. It would be the first manned Buran flight; the third orbiter was the first outfitted with life support systems and ejection seats. Two cosmonauts would deliver the 37KBI module to Mir, using the Buran manipulator arm to dock it to the station's Kristall module. Final crew selection had still not been made at the time the program was cancelled.

  • 1994 December 20 - Mir News 240: After Euromir94 and the docking of the freighter. 

    Progress-M25 there have been no important operations. During the last 10 days the passes for our position took place at night. Meanwhile these passes shifted to the early evening. There has been radio traffic during the night hours about power supply problems. This time the solar panels are not to blame, but the accumulators full of age after 8 years continuous loading and unloading, are no longer able to fulfil their task properly. Now and then they cannot deliver enough power to keep important systems in operation. Sometimes this even causes malfunctions of the gyrodynes.

    Spacewalks (EVA-s): The long awaited EVA's have been put back again. The EVA in which Viktorenko and Polyakov have to replace a docking system inside the transition section obviously is no longer on schedule. The important EVA for the transfer of the solar panels of Kristall to Kvant-1 has been put back to May 1995.

    Communications: The geostationary Kosmos-2054 (Altair) on 16 degr. West is still operational but seldom in use for Mir-TsUP traffic. Sometimes the channel on 10.835 GHz is in use for other 'customers'. Possibly the Russians use another channel for Mir-TsUP communications. On 16.12.94 at abt. noon a new geostationary satellite, Luch-1 has been launched from Baykonur. This Luch-1 will be used for Mir-TsUP communications over 95 dgs East. Possibly this satellite will be operational in January 1995. Long ago 95 dgs East was in use for Luch satellites (Cosmos- 1700 and 1897). For the Russians it would be very useful to place a 2d Luch on 160 dgs. West. Luch-1 on 95 dgs East will help to fill up the gaps after the loss of the tracking stations in Tblisi and Yevpatoriya. There still is a third tracking station near Russia's weak underbelly: Dzhusaly not far from Baykonur, but the status of this station is vulnerable as it is located in Kazakhstan. A lot of unpleasant events during the last years proved that this country does not always appreciate the Russian presence on its territory.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 January 11 - Mir News 241: Autonomous test flight Soyuz-TM20. 

    On 11.01.1995 between 0900 and 0925 UTC the Soyuz-TM20 flew autonomously to test the Kurs-approach and docking system at the forward transition section (P.Kh.O.) of the Mir-complex. Problems during some docking operations in Aug/Sept 1994 (Progress-M24) and on 6.10.1994 (Soyuz-TM20) made this operation necessary. Long before Soyuz-TM20 separated from the complex the whole crew was on board of that ship and thoroughly tested all systems. According to the plan the Soyuz-TM20 executed the approach and docking fully automatically by use of the Kurs system. Viktorenko, assisted by Kondakova, was ready to take over manually if something went wrong or in case of a too high fuel consumption. Soyuz-TM20 perfectly linked to the station at 09.24.57 UTC, the aberrations remained far within the limits, just before docking less than 0.5 degrees. The good functioning of the Kurs systems is indispensable for the execution of the program for this year. During the operation with the Soyuz-TM20 the radio traffic went via the geostationary Altair. During the separation Soyuz-TM20 flew within our range and the traffic could be monitored on 121.750 mc as well as via Altair.

    Luch-1:

    This geostationary satellite to be used for Mir-TsUP communications in the near future is standing over 95 degrees East, but is not yet operational for TDRS purposes.

    Chris van den Berg, NL-9165/A-UK3202

  • 1995 January 26 - Mir News 242: Mir. 

    The Mir-crew is still struggling along to keep the complex habitable and operational. Recently they had to cope with technical problems with the heating, drinking-water, pressure control and with a leakage of water in the Kristall-module. With the help of advice from experts on earth they solved the problems. On 23.01.1995 during the pass in orbit 51032, 0719- UTC, TsUP gave Viktorenko attitude control data to adjust the attitude of the complex in such a way that the solar panels of the Kristall module could deliver a maximum of energy. Dr. Polyakov continued his medical checks and experiments. On request by experts on earth the crew filmed and observed the areas of Kobe in Japan and Grozny. On 21.01.1995 they transmitted these images to earth. It was not always possible to do this due to clouds and bad weather in the areas of interest. Also on 21.01.1995 Dr. Polyakov gave a lecture for Russian children, members of an organisation for young people interested in spaceflight. During a long TV-session via Altair Polyakov explained how the systems in the base block worked. Extensively he explained all about the production and delivery of oxygen for the complex and the purification of the air on board. He emphasised the necessity of the permanent survey of the life systems and a regular maintenance.

    Rendezvous Discovery (STS-63) with Mir: On 2.02.1995 at 0549 UTC STS-63 will be launched for a flight in which the most important operation will be a rendezvous with the Mir-complex. Somewhat earlier, on 4.02.1995 at 1221- UTC Mir and Discovery will be able to establish radio contact. From Discovery cosmonaut Titov and the female astronauts Collins and Voss will speak with the crew of Mir. On 5.02.1995 at 1828 UTC the rendezvous operation will begin and STS-63 will approach Mir in a distance of 10 meters.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 February 3 - STS-63.  Spacecraft: Discovery. Mass: 8,641 kg (19,050 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Deployed ODERACS 2A-2E; deployed and retrieved Spartan 204. Discovery rendezvoused with Russia's space station, Mir, to a distance of 11 m and performed a fly-around, but did not dock with Mir. Payloads: SPACEHAB 03, Shuttle Pointed Autonomous Research Tool for Astronomy (SPARTAN) 204, Cryo Systems Experiment (CSE)/GLO-2 Experi-ment Payload (CGP)/Orbital Debris Radar Calibration Spheres (ODERACS) 2, Solid Surface Combustion Experiment (SSCE), Air Force Maui Optical Site (AMOS), IMAX Cargo Bay Camera (ICBC)

  • 1995 February 11 - Mir News 243: Discovery-Mir. 

    The rendezvous operation got sufficient attention in the media. So I refrain from repeating the extensively published facts. I monitored as much as possible radio traffic related to the rendezvous. Here some items which might be interesting for insiders and 'real spaceflight freaks': 1. During the rendezvous TV transmissions from Mir with images of Discovery were relayed via Altair, the Russian TDRS over 17 degs. West. These transmissions reached K.S.C. and Houston and have been widely used by TV-organisations, for instance CNN. As soon as the windows for Mir-Altair traffic closed the new Luch-1 over 97 degrees East and a number of Russian tracking stations took over. 2. Co-operation and co-ordination between both FCC-s (Houston and Kaliningrad) went smoothly. 3. For direct radio contact between Mir and Discovery the VHF- channels 121.750 and 130.1625MC -in fact Mir-channels- were in use. Vladimir Titov also used a handset for communications in the ham band: 145.325 and 145.625Mc. Before and after the rendezvous operation Mir and Discovery now and then used Altair and TDRS channels for contact with each other. 4. Regularly commentators emphasised the fact that the operation was a rehearsal for the docking operation of Atlantis in June 1995. This rehearsal was a success: Discovery remained stable on the closest approach of 10 M just in a position opposite to the docking port of the Kristall-module to be used by Atlantis for the docking. Before that docking the Russians will have to move the Kristall from the side- to the axial forward docking port of the transition section.

    Radio traffic during the days before the launch of Discovery and before the rendezvous: A lot of traffic was related to the preparations of the rendezvous. For the Mir-crew this meant a lot of work to install TV- and Photo camera's and training in communication procedures. Conversations about these subjects could be monitored during communication sessions via Altair. Also via Altair the Mir-crew regularly spoke with cosmonaut Titov on K.S.C. where he was waiting for the launch.

    After the rendezvous: Unfortunately the passes of Mir and Discovery for our position occurred during the night hours and the cosmonauts stuck to their normal day- and night routine. This made it impossible for us to monitor direct radio traffic between Mir and Discovery being not far from each other for a long time. During all possible windows for visual observations dense clouds made these observations impossible.

    Mir-routine now: Now the Russians are again among themselves. This will not often be the case in 1995 and 1996. (To be continued in the next MirNEWS).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 February 11 - Landing of STS-63. 

    STS-63 landed at 11:51 GMT.

  • 1995 February 12 - Mir News 244: Mir-routine. 

    Mir's passes within our range are gradually shifting to the late evening hours. So the number of VHF- sessions will increase. During the day hours the Russians regularly, though a little bit frugally, use the Altair satellite for Mir-communications. During a long session on 8.02.95, orb. 51281, 0824-0853 UTC, Polyakov was training at the controls of Soyuz-TM20. By the use of the test possibilities without activation of the systems Soyuz-TM's can be used as link trainer. In fact steering of such a ship is not the task of the physician-cosmonaut, but useful if this unexpected might be necessary in emergency situations. Polyakov had a rough time during this exercise for towards the end everything went wrong. On the same day during orb. 51284, 1437-1500 UTC, Mir spoke with the crew of Discovery via Altair and an American TDRS. Polyakov congratulated the Discovery crew with the successful deployment of the satellite Spartan. On 11.02.95 , orb. 51327, 0829-0913 UTC, Polyakov assisted by Kondakova gave a lecture for a group of spaceflight loving children about food on board the Mir complex.

    Progress-M27: The launch from Baykonur of this freighter is on schedule for 15.02.1995 at 1647 UTC. If all goes according to plan Progress-M27 can be monitored in our vicinity (Western Europa and UK) that day at about 1950 UTC. Frequencies: 922.755, 166.130, 166.140 and 165.873 MC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 February 15 - Progress M-26.  Spacecraft: Progress M. Mass: 7,139 kg (15,738 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 17 Feb 1995 18:21:34 GMT. Undocked on 15 Mar 1995 02:26:38 GMT. Destroyed in reentry over the Pacific Ocean on 15 Mar 1995 06:15:00 GMT. Total free-flight time 2.22 days. Total docked time 25.34 days.

  • 1995 February 15 - Mir News 245: Progress-M26 launched. 

    Correction on MirNEWS.244 Read Progress-M26 instead of Progress-M27.

    Progress-M26 launched:

    The freighter Progress-M26 has been launched from Baykonur on 15.02-

    .1995 at 164827 UTC. During the pass between 2252 and 2259 UTC the transmissions in the 166, 165 and 922 Mc band could be monitored. Progress-M26 has to deliver new supplies to the Mir station, i.e. water, fuel, oxygen, oxidisers, food, but also materials for the extension of the on board systems, repair material for the drinking water installation, post and a new board documentation, medical goods, underwear etc. and an amount of 132 KG hard- and software for the experiments of the American Thagard. The enormous cargo made it impossible to equip Progress-M26 with a VBK (ballistic return capsule). Progress-M25: This freighter will separate from Mir on 16.02.1995 at 1303 UTC and will be deorbited at 1606 UTC for decay in the atmosphere over the Pacific. In this way the aft (Kvant-1) docking port of the complex will be made available for the arrival of the Progress-M26.

    Estimated docking time: Progress-M26 has to dock to the Mir station on 17.02.1995 at 1821 UTC.

    Mir: On 10.02.1995 at 183542 UTC the orbit of Mir has been corrected a little bit. With an impulse of 2m/sec the period changed from 92.3 mins to 92.39 mins. New Keplers: Epoch 95043.6810782, decay rate: 0.00046585, incl 51.6467, raan 61.6530, ecc. 0.0005015, arg per 116.1404, ma 244.1203, mm 15.57626647, rev. nr. 51354.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 February 17 - Mir News 246: Successful docking Progress-M26 at Mir. 

    Freighter Progress-M26 docked at the aft (Kvant-1) docking port of the Mir-complex on 17.02.1995 at 182136 UTC in orb. 51427. Approach and docking took place in the automatic mode with the system Kurs. Viktorenko was ready to take over manually (by TORU) if necessary. He reported the movements of the Progress-M26 which enabled me to monitor the operation until 'kasaniye' (touch, soft docking). For TV-transmissions and phone the Russians used the geostationary Altair. This time the docking was executed in the earth's shadow. A searchlight had been installed on the Progress-M26. During the next orbit (0912 UTC) the crew reported that the airseal was good. It lasted a long time before the crew could enter the Progress-M26 due to some obstructing goods.

    Decay of Progress-M25: Progress-M25 left the aft docking port on 16.02.1995 at 1303 UTC. After two autonomous orbits the Progress-M25 got an impulse at 1606 UTC to enter the dense layers of the atmosphere. She decayed in a for that purpose designated area over the Pacific East of New-Zealand. Progress-M25 did not carry a VBK (ballistic return capsule). The Russians do not equip Progress-M ships with such a capsule if the landing has to take place in the winter.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 March 14 - Soyuz TM-21.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-18. Soyuz TM-21 carried the EO-18 Mir crew and American Norman Thagard. Thagard was the first American to be launched in a Soyuz. Soyuz docked with Mir at 07:45:26 GMT on March 16 . On July 4 Soyuz TM-21 undocked and backed off to a distance of 100 m from Mir. The US space shuttle Atlantis, with the EO-18 crew aboard, then undocked and began a flyaround at a distance of 210 m, while the EO-19 crew aboard Soyuz took pictures before redocking with the station. Soyuz TM-21 again undocked with the EO-19 crew on September 11 from the Kvant rear port on Mir and landed at 50 deg 41'N 68 deg 15'E, 108 km northeast of Arkalyk in Kazakhstan, at 06:52:40 GMT .

  • 1995 March 16 - Mir News 247: Flight of Soyuz-TM21. 

    Launch from Baykonur on 14.03.1995 at 0611 UTC; docking to the Mir-station on 16.03.1995 at 0745 UTC. The crew consisting of the captain Dezhurov, board-engineer Strekalov and the American Norman Thagard, uses the call Uragany, so resp. Uragan-1, 2 en 3. All went well during the 2-days flight. During the 4th and 5th orbit Soyuz-TM21 had been corrected and the crew reported this on 121.750 mc during passes within our range. Telemetry- and beacon-transmitters could be monitored on the well known frequencies (166.130, 165.873 en 922.755mc.). To communicate with TsUP Soyuz-TM21 had to be within range of the ground stations in Russia and Kazakhstan. Communications via the geostationary satellites Altair and Luch-1 are only possible when an Soyuz-TM21 is within range of the Mir-station. Then Mir can act as a relay station. This can be heard during the pass within our range just before the docking. The signals from the Soyuz-TM can be received simultaneously: directly on 121.750 mc as well as via Altair. The images used by American TV-stations reached them via Mir and Altair. The TV-report from Soyuz-TM21 from CNN ceased when Mir/Soyuz-TM21 left the window for Altair. The crew of the Soyuz-TM21 seemed to have no adaptation problems, Strekalov and Thagard have a lot of experience, but newcomer Dezhurov also performed his tasks well. Mir: The crew has been very busy with preparations for the arrival of the so called 18th Main Expedition to Mir. Life support systems and other vital equipment got special attention. As usual before the oncoming return the crew had to undergo a lot of medical checks (E.C.G.-s etc.). The crew also completed the work with the freighter Progress-M26, due to leave the aft docking port of the complex for that port must be available for the docking of the Soyuz-TM21.

    Progress-M26 separated from Mir on 15.03.1995 and decayed that day in a designated area East of New Zealand at abt. 0600 UTC.

    Return to Earth of the 17th Main Expedition (Viktorenko, Kondakova and Dr. Polyakov) on 22.03.1995 with the Soyuz-TM20.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 March 22 - Mir News 248: Soyuz-TM20 returned to Earth. 

    The Soyuz-TM20 made a safe landing at abt 50 KM from the city Arkalyk in Kazakhstan on 22.03.1995 at 0405 UTC. Soyuz-TM20 landed only 10KM from the estimated aiming point. The return operation was executed as planned: On 21.03.1995 at 2135 UTC closing of the hatches, 22.03.1995 at 0040 UTC separation from the Mir- station, 0315 UTC starting engines to reduce speed to start descent and a safe landing at 0405 UTC. In the hour before the landing (between 0306 and 0349 UTC) radio traffic of Soyuz-TM20 with TsUP via Mir and Altair could be monitored. Viktorenko and Kondakova reported the operational data, Kondakova having the lion's share. Emancipation as far as spaceflight is concerned has been successfully concluded! Separation of motor compartment and life compartment at 033955 UTC. Just before re-entry the ANAN-rescue beacon could be heard. From 0340 UTC radio silence caused by the plasma-heath.

    Records:

    Dr. Polyakov fulfilled 438 days in space during 1 flight, so 72 days more than Titov and Manarov (366 days at a stretch). Kondakova was 169 days in space.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 March 22 - Landing of Soyuz TM-20. 

    Soyuz TM-20 landed 22 km northeast of Arkalyk in Kazakhstan at 04:04 GMT with crew of Viktorenko, Kondakova and Polyakov aboard.

  • 1995 April 6 - Mir News 249: Progress-M27. 

    On 9.04.1995 at 2133 UTC this freighter will be launched from Baykonur for a flight to the Mir-space station. If all goes according to plan the ship will dock at the for ward (P.Kh.O.) port on 11.04.1995 at abt 2058 UTC. Approach and docking will be in the automatic mode by the system Kurs. The captain of Mir is ready to take over manually by the TORU system in case of problems during the automatic approach.

    ALTERATIONS:

    During the Mir's pass over here during orb. 52158, on 5.04.95 TsUP informed the crew about some alterations of the recent planning: 1. Immediately after the arrival of Progress-M27 the cosmonauts will have to work on the gyrodynes. This on request by the Americans. In their opinion the complex needs 12 well functioning gyrodynes. This means that the first EVA planned for 28.04.95 will be put back to the beginning of May, possibly to 1.05.95. 2. The launch of the module Spektr on schedule for 10.05.95 has been put back to 20.05.95. One of the causes of this delay is the installation of equipment on Spektr to make the use of the system TORU by the Mir-crew possible if during the docking operation the automatic system Kurs fails. 3. Though not confirmed thus far the delay of the launch of the Spektr might also put back the launch date of the Atlantis for the docking mission by appr. 10 days.

    GFZ-1: Progress-M27 also has to deliver to the Mir-complex the normal cargo (food, fuel, water, spare parts, experiments, etc.) a small satellite named GFZ-1. GFZ-1 is a spherical satellite with a mass of 20 KG and a diameter of appr. 20 CM. GFZ-1 has been constructed by the German firm Kayser-Threde (Munchen) and will be used by the Geoforschungszentrum Potzdam for geodetic experiments by laser reflectors. GFZ-1 makes it possible to deliver highly accurate measurements of the Earth's gravitation field. Shortly the Mir-crew will launch GFZ-1 for its autonomous flight of appr. 2 years.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 April 9 - Progress M-27.  Spacecraft: Progress M. Mass: 7,170 kg (15,800 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir; carried GFZ-1 German sub-satellite to Mir. Docked with Mir on 11 Apr 1995 21:00:44 GMT. Undocked on 22 May 1995 23:42:37 GMT. Destroyed in reentry on 23 May 1995 03:27:52 GMT. Total free-flight time 2.22 days. Total docked time 41.11 days.

  • 1995 April 12 - Mir News 250: Progress-M27. 

    This freighter started from Baykonur on 9.04.95 at 1933 UTC. After a 2-days flight during which no problems emerged Progress-M27 docked to the forward (P.Kh.O. - transition section) of the Mir complex on 11.04.1995 at 2100 UTC (21 hrs 00 mins 42 seconds), so on 12.04.1995 at 0100 Moscow Summer Time. Approach and docking took place in the automatic mode by the system Kurs. Dezhurov was ready to take over manually by the remote control system TORU, but this was not necessary. Progress-M27 docked during Mir's orbit 52262. During the final approach and docking traffic was relayed by Altair. There were no TV-images. Dezhurov reported details of the approach and the soft docking (kasanye). During the next pass in orb. 52263, at 2227 UTC Strekalov reported that they had opened the hatch to Progress-M27 2 minutes earlier and that everything was in good order. Progress-M27 delivered to the complex the normal cargo (water, food, fuel, post, underwear, scientific material, etc.), repair materials for the systems to maintain a good atmosphere and the water generation and the German micro-satellite GFZ-1.

    GFZ-1: So this little satellite is now on board of the Mir- complex waiting for its 'second' launch. This has to be done by the cosmonauts in the night from 19 to 20.04.1995. This spherical object with a mass of 20 KG and a diameter of 21 CM will separate from Mir with a speed of 1.2 M/sec. During this operation the German tracking station Oberpfaffenhofen will play an important role. (For details about GFZ-1 see Mir-

    NEWS.249)

    During the pass in which Strekalov reported the opening of the hatch, TsUP told him that the first EVA will take place on 11.05.1995. The date for the launch of Spektr (thus far on schedule for 20.05.1995) might be changed. After the launch of the Spektr, so during one of its 7-days autonomous flight, Progress-M27 will be separated from Mir.

    Possible launch date of Atlantis for the flight in which she has to dock to Mir: 22.06.1995. If so the flight of the Disco very might be put forward to 6.06.1995. This all is not sure at this moment.

    C.M. van den Berg, NL-9165/A-UK3202.

  • 1995 April 19 - GFZ-1.  Spacecraft: GFZ-1. Mass: 20 kg (44 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Geodetic; carried retroreflectors for ground laser ranging; delivered to Mir on Progress M-27 and deployed from Mir 4/19/95 .

  • 1995 April 20 - Mir News 251: GFZ-1 launched by Mir-crew. 

    On 19.04.1995 at 1912 UTC this spherical microsat (21 CM diameter, mass 20 KG) has been pushed into space from an airlock of Mir's base block. GFZ-1 moved off with a speed of 1.2 M/sec. The traffic in which the reports of data and images of the autonomous GFZ-1 could be monitored via Altair. The same operation had taken place some days before: On 17.04.1995 at 08Hrs 19Mins 50Secs the crew launched a container with garbage to be sure that the system would work well. This object is now in space under catalogue number 23557. GFZ-1 has been built by the German firm Kayser-Threde. The co-ordination of the observations of GFZ-1 will be done by the Geoforschungszentrum Potsdam. Abt 25 observatories all over the world will execute measurements by laser reflections. Stations are among others: London, Grasse (France), Potsdam, Easterisland, Graz (Austria) and even one in Kirgizie. The stations can 'catch' GFZ-1 with a beamwidth of 200 Meters. During the first pass London and Graz did not get reflections, but during the 2d pass Graz caught GFZ-1 and was able to pick the first geodetic and ballistic measurements. During the launch the Mir-crew acted independently.

    Planning for the near future:

    Some crucial operations had to be put back by the Russians (launch module Spektr, EVA-s, a.s.o.) and this forced the Americans to put back the launch of the Atlantis to the second half of June. Therefore the flight of Discovery has been put forward and will now begin at abt 8.06.1995.

    Cargo Progress-M27: An antenna for radio-amateur purposes, delivered by Progress-M27, has been damaged due an improper packing. The crew showed this antenna via Altair and discussed this problem with the well known radio-amateur Sergey Samburov.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 May 8 - Mir News 252: Spacewalks (EVA-s). 

    The data for the 1st two EVA-s are: 12 and 17.05.1995. After these 2 EVA-s there will be made another 2 of which data and other details still have to be settled. There is a possibility of 2 extra, so called 'contingency' EVA-s. The EVA on 12.05 will begin at 0500 UTC (opening of the hatch), last abt 5 hours and the main task will be the transfer of a solar panel from Kristall to Kvant-1. Possibly the cosmonauts will also retrieve materials which have been exposed to open space. During radio communications in the last week could be heard how the cosmonauts checked systems, spacesuits, communication channels, etc. The last 2 days these checks were focused on the communication channels. The checks were very realistic and gave a good insight in the communications procedures and systems. During EVA-s the 143.625 shifts to 143.617 mc, so lower than the normal Doppler shift and interference by an air traffic channel are standard and during those checks the same happened. Preparations for the 1st EVA will begin in the night from 11 to 12.05.1995, the opening of the hatch, in fact the beginning of the EVA, will be at abt. 0500 UTC. The Russians Dezhurov and Strekalov will do the EVA, Thagard will be on duty in the Mir- complex.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 May 12 - EVA Mir EO-18-1.  Spacecraft: Mir.

    Retracted solar array.

  • 1995 May 12 - Mir News 253: 1st Spacewalk (EVA). 

    Today the cosmonauts Dezhurov and Strekalov had their first EVA during this expedition. Strekalov made EVA's in the past; for Dezhurov it was his first. The hatch has been opened at 0420 UTC and closed at 0935 UTC. So the duration of this EVA was 5 hrs 15 mins. The cosmonauts executed 3 tasks: 1. To install cables and contacts on Kvant-1 for the electric power of the solar panel to be installed there during the 2nd EVA. 2. To check whether it is possible to roll up that solar panel which still is installed on Kristall for the transfer to Kvant-1 during the 2d EVA. This was possible. 3. The retrieval of materials which have been exposed to open space for a long time (the American experiment Trek). The 2d EVA will be executed on 17.05.1995. Then the 1st solar panel definitely must be replaced from Kristall to Kvant-1. During the spacewalk Norman Thagard was on duty inside the station to look after the communications and now and then giving commands, for instance the switching off and on of the power of the solar panel during the work on it by the cosmonauts. For communications between TsUP and Mir all available windows for traffic via Altair have been used.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 16 - Mir News 254: 2d Spacewalk (EVA) Mir-crew. 

    The crew of the 18th Main Expedition, Dezhurov and Strekalov, will do their 2d EVA on 17.05.1995. This EVA will begin at 0247 UTC (opening of the hatch) and will end at 0820 UTC (closing the hatch.) The cosmonauts will fold up and transfer one of the solar panels of Kristall (Module-T) to the outer surface of the astrophysical module Kvant-1. They will use the Strela- crane as a lever. The cosmonauts have to make complicated manoeuvres with Strela: they have to reach the Kristall module first and later on swing over to the Kvant-1 with their 'car go'.

    The American astronaut, Norman Thagard, will stay inside the complex and execute commands if necessary. Today he even practised the loading of date in the movements computer of the complex.

    1st EVA (correction and completion):

    At the moment of the closure of the Altair/Mir window on 12.05.95 at 0937 UTC I was sure that the EVA was still going on. However I believed a spokesman who stated that the hatch had been closed at 0935 UTC. In fact the EVA lasted 1 hour longer until 1035 UTC (1335 TsUP Time and not Moscow summertime) so exceeding the planned EVA with 1 hour and the guaranteed security period for the spacesuits with 15 minutes. The cosmonauts were very tired when they came back on board, but satisfied for the EVA was a success.

    Launch of Spektr: Still on schedule for 20.05.1995.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 17 - EVA Mir EO-18-2.  Spacecraft: Mir.

    Began installation of solar array.

  • 1995 May 17 - Mir News 255: 2d Spacewalk (EVA) Mir crew. 

    The Russian crew members of the 18th Main Exp. to Mir, Duzhurov and Strekalov, did their 2d EVA on 17.05.1995 from 0238 until 0930 UTC. This EVA also lasted longer than planned and again the 'safety guarantee period' has been exceeded. During this EVA the cosmonauts had to fold up the solar panel on Kristall, to disconnect contacts and drivers, install the 'cargo' on the Strela crane en transport this and Strekalov to Kvant-1. Strekalov folded the panel assisted by Thagard who was inside the complex and gave commands to switch off and on servomotors. After every 'movement' caused by these servo's Strekalov could fold the next section. Str worked on the panel, Dezhurov steered the Strela. For the 'fold-up' operation the cosmonauts used more time than was expected. They also spent a lot of time to reach the necessary spots. The cosmonauts could not fully accomplish their task due to the limited endurance of their spacesuits. They left the package behind on the outer surface of Kvant-1 and returned to the airlock. During the beginning of the operation communications were relayed via Altair, later on and within our range the 143.625 mc was active. As always during EVA's interference by cross-modulation from an air traffic control channel. During the first pass after the EVA the cosmonauts could be monitored waiting in the airlock for the equalisation of the air pressure.

    3d EVA: To accomplish their task the cosmonauts will make their 3d EVA on 24.05.1995. Orbit correction: On 15.05.1995 at 0630 UTC Mir's orbit has been corrected. This correction was necessary to make the docking of Atlantis to Mir late June this year possible. Herewith the most recent Keps: Epoch: 135.39591536, decay: 0.00024944, Incl: 51.6461, RA: 321.7764, Ecc.: 0.0005314, Arg. per.: 307.8737, MA: 51.1567, MM: 15.56501886, Rev. nr.: 52784.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 18 - Mir News 256: Intercalated Spacewalk (EVA). 

    During their 2d EVA on 17.05.1995 the cosmonauts were not able to accomplish their task due to a threatening lack of oxygen. This EVA was the 2d one in a series of 4. There was a possibility to use 2 so called 'contingency-EVA's'. The first of these contingency EVA's will take place on 22.05.1995. The time of the opening of the hatch and the duration are still unknown. This EVA -so now to be counted as the 3d one- will be made to complete the transfer of a solar battery from Kristall to Kvant-1 (37KE). The cosmonauts will have to install, deploy and activate that solar panel. To fill up the gap in the energy supply the solar panels of the freighter Progress-M27 are now also delivering energy to the Mir-complex. Thus far is not known when the EVA on schedule for 24.05.1995 will be made.

    Launch of Spektr:

    The Spektr technological module will be launched by a Proton carrier from Baykonur on 20.05.1995 at 0330 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 20 - Spektr.  Spacecraft: Spektr. Mass: 19,640 kg (43,290 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    MIR experiment module. Docked to Mir Jun 1
    Officially: Docked to Mir Jun 1

  • 1995 May 22 - EVA Mir EO-18-3.  Spacecraft: Mir.

    Completed installation of solar array.

  • 1995 May 22 - Mir News 257: 3d Spacewalk (EVA) Mir-crew on 22.05.95. 

    The EVA lasted from 0010 UTC (opening of the hatch) until 0525 UTC (closing of the hatch). The cosmonauts installed, connected, unfolded and activated the replaced solar panel. A hell of a job aggravated by limited communications with TsUP. The original planning spoke about the use of almost all windows via Altair during the EVA, but this was not possible due to lack of power. After the 2d EVA there had been no traffic via Altair for the same reason. Immediately after the installation of the solar panel on Kvant-1 traffic via Altair could be monitored. After the return of the cosmonauts on board there was a TV-session in which the installed solar panel, the Strela and the Sofora mast with the VDU were shown.

    4th EVA: This very short (40 minutes) EVA will take place on 29.05.1995. During this EVA a docking cone will be moved from the -Y axis port to the -Z axis port. This for the docking of Spektr on 1.06.1995. After some time the Spektr will be moved 90 degrees to one of the X-axis ports to make place for the Kristall to be placed on the -Z axis port to enable the Atlantis to dock in June.

    Progress-M27: This freighter remained 2 days longer at Mir to help reduce the lack of power of the Mir-complex. Possibly Progress-M27 will be undocked on 22.05.95 at 2332 UTC and burn up over the Pacific West of New Zealand on 23.05.95 at about 0328 UTC.

    SPEKTR: This huge module (20 tons) has been launched from Baykonur on 20.05.1995 at 03.33.22 UTC and will dock to Mir on 1.06.1995. This to enable the Mir-crew to make their 4th EVA. On 21.05.1995 Spektr came in a higher orbit by 2 motor burns: 1st: 0211 UTC (6.4 M/sec.) 2d : 0419 UTC (15.0 M/sec) The following motor burns have been scheduled for 24.05.1995: 1st: 003625 UTC (15M/sec). 2d : 023510 UTC ( 3M/sec).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 23 - Mir News 258: Progress-M27 separated from Mir and decayed. 

    The freighter Progress-M27 undocked from Mir on 22.05.1995 at 23.29.30 UTC and decayed over the Pacific East of New Zealand on 23.05.1995 at 03.27.12 UTC.

    Spektr: The forward axial docking port of the P.Kh.O. (transition section) is now free for the reception of Spektr on 1.06.1995.

    4th Spacewalk (EVA): Still on schedule for 29.05.1995. (Transfer inside P.Kh.O. of docking device from -Y to -Z. (Duration abt. 40 minutes).

    5th EVA: On 2.06.1995 the 5th EVA will be made. Purpose: adjustments inside P.Kh.O. in relation to oncoming redockings of Spektr and Kristall. (Duration: short)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 May 26 - Mir News 259: Schedule for operations in period from 26.05 until 3.06.1995.. 

    Redocking of Kristall module from -Y axis to -X axis:

    In the night from 26 to 27.05.95. Period: from 26.5 2309 UTC to 27.05.95 at 0040 UTC. (-X axis is forward port transition section, P.Kh.O.)

    4th Spacewalk (EVA):

    This EVA will take place on 28.05.95 from 2240-2310 UTC (in Moscow time already 29.05.1995). The cosmonauts will remain inside the vacuumed P.Kh.O. (transition section) for the replacement of the docking cone from the -X axis to the -Z axis. This for the temporary 'parking' of the Kristall.

    Redocking of Kristall from the -X axis to the -Z axis on 29.05.1995 from 2200-2330 UTC (in Moscow time already 30.5). The forward docking port (-X axis) is then free for the reception of Spektr.

    Docking of Spektr is planned for 1.06.1995 at abt 0038 UTC. Koppeling van de Spektr aan het Mir-station:

    The 5th EVA will take place on 2.06.1995, again fully within the P.Kh.O. with a duration of abt. 40 mins. Beginning time thus far unknown. During this EVA the cosmonauts will replace the docking cone from the -Z axes to the -Y axes. This to make redocking from Spektr to that port possible.

    Redocking of Spektr from the -X axes to the -Y axis will take place on 3.06.1995 (times thus far unknown).

    When the Kristall will be redocked from the -Z axes to the -X axes is unknown thus far, but Kristall has to be positioned to that port for the docking of the Atlantis.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 May 28 - EVA Mir EO-18-4.  Spacecraft: Mir.

    Repositioned docking adapter.

  • 1995 June 1 - EVA Mir EO-18-5.  Spacecraft: Mir.

    Repositioned docking adapter.

  • 1995 June 1 - Mir News 260: SPEKTR linked up with the Mir-complex. 

    The 20-tons technological module Spektr docked automatically and without any problems at the forward docking port (-X axis) of the transition section (P.Kh.O.) of Mir on 1.06.1995 at 00.56.16 UTC. During the pass within our range in orb. 53043 from 0046-0052 UTC the transmissions of both object could be monitored. At 0048 UTC Strekalov reported the distance to Spektr: 15 meters. He also stated that the final approach was about to begin. TsUP ordered the crew to do camerawork and so it might be possible that we somewhere can see some images (media and editors permitting). During the pass in orb. 53044 from 0223-0229 UTC the crew got orders to observe an operation with a solar panel: this had to be folded or retracted to become a little bit shorter. There were no remarks about the opening of the hatches to Spektr. During the following passes the crew slept. This successful docking means that the major obstacle on the way to the docking of Atlantis in the 3d decade of June has been taken. The arrival of Spektr is very important for further Mir operations and the co-operation with the Americans not only for the module itself but also for the indispensable cargo to be delivered by Spektr.

    Results of the operations as of 27.05.1995:

    All operations have been carried out successfully in accordance with the schedule published in MirNEWS.259. So the Kristall module has been redocked twice (from the -Y to the -X axis and from there to the -Z axis). The Russians are satisfied about the good functioning of the manipulator arm (the so called 'lyappa'), which has not been tried out in the 5 years after the redocking of Kristall from -X to -Y in June 1990.

    Plans for the next 7 days:

    During the night from 1 to 2.06.1995 a short spacewalk (EVA) inside the vacuumized transition section (P.Kh.O.) to replace the docking- (reception-) cone from the -Z to the -Y axis.

    In the night from 2 to 3.06.1995 the redocking of Spektr with its 'lyappa' from the -X axis to the -Y axis.

    On 7.06.1995 Kristall will be redocked to the -X axis to be ready for the reception of Atlantis in the 3rd decade of June.

    Chris v.d. Berg, NL-9165/A-UK-3202.

  • 1995 June 5 - Mir News 261: 5th Spacewalk (EVA) Mir-crew. 

    On 1.06.1995 (for Moscow time already 2.06.1995) from 2204- 2229 UTC the Mir-crew made a short EVA inside the vacuumized transition section (P.Kh.O.). During this EVA they replaced the docking cone from the -Z to the -Y axis.

    Redocking Spektr (Module-O):

    This operation was executed quickly and successfully (so also the 'Lyappa' of Spektr is reliable) on 2.06.95 from 1952- 2150 UTC (so the closing of the hatch already on 3.06.95 Moscow time). The Spektr has been moved from the -X axis (axial forward port of Mir) to the -Y axis. So the forward port is now available to receive the Kristall (Module-T). Redocking of Kristall put back:

    This operation was on schedule for the night from 6 to 7.06.1995 but has been postponed to the period from 15.06 - 18.06.1995. The Russians said that this was necessary due to activities with a higher priority. It might be possible that this has something to do with the airseal problems arose after the redocking of Kristall in the night from 29 to 30.05.1995. That night during the pass in orbit 53012 Dezhurov reported a dropping pressure in Kristall or the transition section (P.Kh.O.). This might be caused by a minor leakage in the joint between Kristall and the P.Kh.O. After 1 hr and 8 minutes the pressure dropped from abt 700 mm to 469 mm. Whether this problem has caused the postponement of the redocking of Kristall has not been confirmed thus far. That there is a problem with the air pressure has been confirmed officially. Spokesmen also stated that extra oxygen en nitrogen has to be delivered to the complex to replenish the loss of air during the recent EVA-s.

    Thagard injured his eye: Not all what is written in my logbook reaches my reports. Already on 19.05.1995 Thagard reported that he injured his right eye during an 'experiment with an expander'. During the days there after Thagard regularly complained about his eye and TsUP advised him which medicines he had to swallow. Meanwhile the eye seems to be recovered for when there is question about this problem Thagard and his colleagues say that all is normal. I did refrain from publishing about this medical 'secret' due to an official request. Recently this ban has been lifted by the Head of the Russian Space Agency, Koptev, who told Itar-Tass that Thagard had been struck at his head above his right eye by a spring which got loose from an expander during physical training.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 June 13 - Mir News 262: Redocking Kristall-module. 

    The air seal problems with the joint between Kristall and the transition section (P.Kh.O.) have been resolved earlier than had been expected and so Kristall could be redocked from the -Z to the -X axis (forward axial port) on 10.06.1995 at 1730 UTC. The operation was accomplished at 1800 UTC. So Kristall is now ready for the reception of the shuttle Atlantis.

    SPEKTR: One of the 4 solar panels not fully deployed.

    One of the solar panels of Spektr did not unfold fully. This malfunction caused power problems and a very scarce use of the communications via Altair. To repair the solar panel the cosmonauts will have to make an extra spacewalk (EVA).

    6th EVA:

    To make the deployment of the solar panel of the Spektr possible the cosmonauts will have to do an EVA on 15.06.1995 between 1400 and appr. 1900 UTC.

    Launch Atlantis:

    The Americans are doing all what is possible to execute the launch of Atlantis on 22.06.1995. The Russians as well as the Americans are sure that the solar panel of Spektr will be repaired in time.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 June 15 - Mir News 263: 6th Spacewalk (EVA). 

    During a meeting at Noordwijk Space Expo Kondakova told me that the EVA planned for 15.06 has been put back to 16.06.95. During radio traffic via Altair on 15.06 during orb. 53268, 0835-0925 UTC the cosmonauts asked for a duration of the EVA of 5.30 instead of 5 hrs. During that EVA they will have to deploy an unwilling solar array on Spektr and to inspect this to be sure that it will give no problems during the docking of Atlantis. They also will have to repair an unreliable drive of a solar array on Kvant-2 (Module-D) and check the docking port of the -Z axis due to the recent air leakage.

    Start Atlantis: When Atlantis will be launched is not yet sure for 100%, but if the EVA will be successful and no other problems emerge NASA intends to execute the launch on 23.06.95 at 2308 UTC (launch window 7 mins). I hope to be on the spot during the launch and landing, which has been planned for 4.07 at 1637 UTC. Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 June 17 - Mir News 264: Planned spacewalk (EVA) cancelled. 

    This EVA already had been put back once from 15 to 16.06.1995, but has now been cancelled. The cosmonauts did not have the right tools for their tasks and doing the job with the tools now at their disposal would be too risky. The Russians and NASA are sure that the present situation (power problems and the not fully deployed solar array on Spektr) is safe enough for the intended docking operation of Atlantis. The EVA will be made by the crew of the next mission (19th Main expedition), Solovyov and Budarin, who will deliver the right tools to Mir and already trained in Houston for that EVA.

    ATLANTIS READY TO GO!!

    After a long period of uncertainties, of hope and despair, the date for the launch of Atlantis on her docking mission has been set: 23.06.1995 at 2108 UTC. Docking on 25.06.1995 at abt 1430 UTC. The launch window is only 7 minutes long and if the launch not takes place in first 2 minutes the flight before docking had to last 3 instead of 2 days. NASA however sticks to the docking on 25.06.1995 and will manoeuvre Atlantis in such a way that this is possible.

    HOWEVER.......:

    The fact that the date for Atlantis's launch has been set means that I will fly to the States to be there during the major events and so I will close my station for a while to continue my work on the spot. I will produce reports of all what will happen for some media in the Netherlands and report my findings after my return in a MirNEWS-summary and in the next issue of the Amasat UK journal Oscar News.

    Goodbye everybody!!

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 June 27 - STS-71.  Spacecraft: Atlantis. Mass: 12,191 kg (26,876 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Mir Expedition EO-19. Transferred Budarin, Solovyov to Mir, returned Soyuz TM-21 crew to Earth. After undocking from Mir on July 4, Atlantis spent several days on orbit, carrying out medical research work with the Spacelab-Mir module in the cargo bay. Payloads: Shuttle/Mir Mission 1, Spacelab-Mir, IMAX camera, Shuttle Amateur Radio Experiment (SAREX).

  • 1995 July 7 - Landing of STS-71. 

    STS-71 landed at 14:55 GMT with the crew of Baker, Dezhurov, Dunbar, Gibson, Harbaugh, Precourt, Strekalov and Thagard aboard.

  • 1995 July 11 - Mir News 265: Resumed. 

    Just returned from the United States, where I was during the launch, docking, separation and landing of the STS-71, Atlantis. Still suffering from 'jetlag' and not back in my normal work-rhythm. But nevertheless here some facts about Mir/Atlantis and the plans for Mir this month.

    Atlantis blasted off from KSC on 27.06.1995 at 1932 UTC. Docking at the Kristall-module on 29.06.1995 at 1300 UTC. 4.07.1995 at 1055 UTC Soyuz-TM21 with Solovyov and Budarin separated from Mir's Kvant-1 module for a photo mission of the undocking of Atlantis. 4.07.1995 at 1110 UTC successful undocking of Atlantis from Mir. 4.07.1995 at 1138 UTC Soyuz-TM21 redocked to Kvant-1. This took place 5 minutes earlier than was planned due to a malfunction of the Ts.V.M.-1 (main computer on board Mir). Solovyov per formed the docking manually while the deviation of Mir was already 10 degrees. 7.07.1995 at 1455 UTC soft landing of Atlantis on the S.L.F. (Shuttle Landing Facility) of Kennedy Space Centre.

    Plans Mir-operations this month: 14.07.1995: 1st spacewalk (EVA): Checking airseal of docking port in -Z before the redocking of Kristall and an attempt to deploy the naughty solar array of Spektr. Beginning of EVA at 0340 UTC, duration somewhat more than 5 hrs. 17.07.1995: Possibly, depending on the results of the 1st EVA, the redocking of Kristall from the -X axis (forward port) to the radial port -Z axis. If so this operation will begin at abt 0200 UTC. There was a 2d EVA on schedule for 18.07 (later put back to 19.07), but possibly this EVA will be cancelled. Depending on the results of the 1st EVA. Progress-M28: If all goes well during the operations mentioned above this freighter will be launched from Baykonur on 20.07. Docking has to take place on 22.07 at the forward (-X) docking port of the complex. More news about the near future: There is an EVA planned on 18.08.1995 to install on the outer surface of Mir experiments among which the Belgian MirAS. This experiment has been brought to Mir by the Spektr module. Euromir'95: The launch of this mission with Soyuz-TM22 has been put back to 1.09.1995. (Gidzenko, Avdeyev and Reiter).

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 July 14 - EVA Mir EO-19-1.  Spacecraft: Mir.

    Repaired solar array. Inspected exterior of station.

  • 1995 July 17 - Mir News 266: 1st Spacewalk (EVA) Mir-19 crew. 

    Solovyov and Budarin made their 1st EVA on 14.07.1995 from 0356-0930 UTC. They fully performed their tasks. They found no pollution or damages on the outside of the docking mechanism of the -Z axis. They deployed the jammed solar array on Spektr with the exception of 1 section. The solar array has now been included in the power supply system of the complex. They also worked at a solar array of Module-D and an antenna.

    Redocking of the Kristall-module:

    Kristall has been moved from the forward port (-X axis) to the side port (-Z axis) on 17.07.1995 between 0230 and 0400 UTC. The redocking took place by the use of the 'lyappa'. a manipulator arm. So Kristall is now in the right position to receive the Atlantis (STS-74) and the new docking module in October 1995. On 17.07.1995 during the pass in orb. 53761 at 0554 UTC Solovyov reported that the airseal of the system after the redocking was normal.

    2d EVA Mir-19 crew:

    On 19.07.1995 between 0050 and 0620 UTC the Mir-19 crew will make their 2d EVA for the installation of the Belgian spectrometer MirAS on Mir's outer surface. Originally this operation was on schedule for 18.08.1995.

    Progress-M28: This freighter will be launched from Baykonur on 20.07.1995 at 0305 UTC for a flight to the Mir-space station. If all goes well this freighter will dock to the station on 22.07.1995 at 0437 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 July 19 - EVA Mir EO-19-2.  Spacecraft: Mir.

    Retrieved TREK detector.

  • 1995 July 20 - Progress M-28.  Spacecraft: Progress M. Mass: 7,125 kg (15,707 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir's front port on 22 Jul 1995 04:39:37 GMT. Undocked on 4 Sep 1995 05:09:53 GMT. Destroyed in reentry on 4 Sep 1995 08:58:55 GMT. Total free-flight time 2.22 days. Total docked time 44.02 days. Two Icons of Saint Anastasia were taken into space aboard the craft and transferred to the Mir station where they remained for about seven months. They were returned to earth, apparently aboard Soyuz TM-22, and later shown in diffent shrines around the world.

  • 1995 July 20 - Mir News 267: 2d Spacewalk (EVA) Mir-19 crew. 

    Solovyov and Budarin made their 2d Spacewalk from 0039-0347 UTC. They did not accomplish their tasks and the EVA was shorter than planned. The thermoregulation in the spacesuit of Solovyov was not working normally. S. got orders to remain in the hatch of the airlock and observe the activities of his crew mate. Budarin did some preparations for the installation of the Belgian MirAS experiment and brought back some materials from Mir's outer surface. (possibly the American experiment TREK).

    PROGRESS-M28 launched for flight to Mir:

    The freighter Progress-M28 blasted off from Baykonur on 20.07.95 at 03.04.40 UTC for a 2-days flight to the Mir-space station. Transmissions of this ship could be monitored a few hours after launch on the known frequencies in the 166, 165, 922 and 926 m/c bands. If Progress-M28 sticks to the timetable she will dock at Mir's forward docking port on 22.07.1995 at 0437 UTC.

    3rd EVA Mir-19 crew:

    To finish the tasks, which they were unable to accomplish during their 2d EVA Solovyov and Budarin will do this EVA on 21.07.95 from 0030-0530 UTC. Radio traffic can be expected via Altair during windows Mir-Altair and on VHF (143.625 and 130.165 mc) during the first pass of Mir for Western-Europa in orb. 53823 from abt. 0520-0529 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 July 21 - EVA Mir EO-19-3.  Spacecraft: Mir.

    Installed Miras spectrometer.

  • 1995 July 22 - Mir News 268: 3d Spacewalk (EVA) Mir-19 crew. 

    This EVA took place on 21.07.1995 from 0030-0605 UTC. The main task of the crew consisted of the installation of the Belgian Spectrometer, MirAS, on the outer surface of the Spektr-module. The EVA was a success and the last to be executed by this crew. During the EVA the geostationary satellite Altair (west) has not been used during all possible windows and if so only for voice communications. The recorded images have been transmitted to earth after the EVA possibly via direct channels or Luch-1. Progress-M28 successfully linked up with Mir:

    On 22.07.1995 at 0440 UTC Solovyov reported 'kasaniye' (touch). During the Altair-window in orbit 53838, so in which the approach and docking took place, only voice communications could be monitored. So no images of the approach. Approach and docking were executed in the automatic mode by the system Kurs. The crew observed the approach of Progress-M28 through portholes.

    Progress-M28 docked to the forward axial port (-X) of the transition section (P.Kh.O.). At 0630 UTC checks of the hard docking and airseal had been completed and the hatch was opened just before 0705 UTC. Progress-M28 delivered to the Mir-complex food, water, fuel and scientific equipment.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1995 August 26 - Mir News 269: Euromir'95. 

    The launch from Baykonur of Soyuz-TM22 is still on schedule for 3.09.95 at 0900 UTC. Soyuz-TM22 will carry the relief crew (the 20th Main expedition) to the Mir-station together with the ESA astronaut, the German, Thomas Reiter. The Russian crew consists of the Mir's captain Yuriy Gidzenko, who will make his first spaceflight, and the board-engineer Sergey Avdeyev, who already made 1 spaceflight. This crew and the stand-in crew flew to Baykonur on 23.08.95 to accomplish their final training.

    Mir: During the past weeks the complex passed during the night hours. Meanwhile the passes shifted to the afternoon en evening hours. The clear skies during the evenings made good visual observations possible. The cosmonauts executed a lot of experiments and repairs. They installed new gyrodynes in Module-D and resolved airseal problems. Probably one or more gyrodyne cases showed leaks. The cosmonauts solved this problem using a lute named 'germetik'. They did this by putting this lute around some leaking electric sockets.

    Scarce information: During the past weeks it was difficult for me to maintain sufficient grip on the Mir-operations. This due to family circumstances, the night passes of the complex and the capricious behaviour of the geostationary satellite Altair. (see File ALTC2054.TXT.)

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 September 3 - Soyuz TM-22.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-20. Crew commander was Yuriy Pavlovich Gidzenko of the Russian Air Force. Flight engineer was Sergey Vasilyevich Avdeev of RKK Energiya, and cosmonaut-researcher was Thomas Reiter of the European Space Agency. Soyuz TM-22 docked with Mir's front (-X) port at 10:29:54 GMT on September 5 and the hatch was opened at 11:01:23.

  • 1995 September 4 - Mir News 270: Soyuz-TM22 launched from Baykonur.. 

    This ship with on board the crew for the 20d Main Expedition to Mir and the Euromir'95 cosmonaut Thomas Reiter started flawlessly from Baykonur on 3.09.1995 at 0900 UTC (for the connoisseurs: 09.00.23.115). The Russians are the captain Yuriy Pavlovich Gidzenko, making his first spaceflight, Sergey Vasilyevich Avdeyev, making his 2d flight. The crew uses the call 'Uran', so for Gidzenko, Avdeyev and Reiter, respectively Uran-1, -2 and -3. The 1st day of the 2 days autonomous flight to Mir passed without any problems. Already during the 3d orbit at 120240 UTC Soyuz-TM22 came within our range. Gidzenko reported the successful check of the manual orientation control system. All went well. During the pass at 1332 UTC Gidzenko, sounding very fit, reported that the first 2 orbit corrections had been performed well. All systems worked without hitches and the health and mood of the crew were excellent.

    Planned linkup with Mir-station:

    If all continues to go according to plan the Soyuz-TM22 will dock at the forward docking port (P.Kh.O. -transition section), the -X axis on 5.09.95 at 1030 UTC. The last phase of the approach will take place within our range during Mir-orbit 54543 from 1018-1025 UTC. In this period we can expect radio traffic on the frequencies: 121.750 Mc (Soyuz-TM22) and 143.625 Mc (Mir). It is not possible to predict whether the old Altair on 17 dgs West will be used or not for this good old 'geo' did not show up since 26.08.95 0824 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1995 September 11 - Landing of Soyuz TM-21. 

    Soyuz TM-21 landed at 06:52 GMT with the crew of Budarin and Solovyov aboard.

  • 1995 October 8 - Progress M-29.  Spacecraft: Progress M. Mass: 7,122 kg (15,701 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Launched into an initial 194 x 242 km x 51.7 deg orbit. Docked with Mir's rear of the Kvant module port on 10 Oct 1995 20:32:40 GMT (Soyuz TM-22 was docked to the front port). Undocked on 19 Dec 1995 09:15:05 GMT. Destroyed in reentry on 19 Dec 1995 16:15:00 GMT. Total free-flight time 2.36 days. Total docked time 69.53 days.

  • 1995 October 20 - EVA Mir EO-20-1.  Spacecraft: Mir.

    Sample cassettes installed in ESEF (European Science Exposure Facility).

  • 1995 November 12 - STS-74.  Spacecraft: Atlantis. Mass: 6,134 kg (13,523 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Rendezvoused and docked with Mir space station on November 15. Delivered the Russian-built 316GK Shuttle-Mir docking module to Mir.Payloads: Shuttle-Mir Mission 2; docking module with two attached solar arrays; IMAX Cargo Bay Camera (ICBC); Glow Experiment (GLO-4)/ Photogrammetric Appendage Structural Dynamics Experiment (PASDE) Payload (GPP); Shuttle Amateur Radio Experiment (SAREX) II.

  • 1995 November 12 - Mir-Shuttle Docking Module.  Spacecraft: Mir-Shuttle Docking Module. Mass: 6,134 kg (13,523 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Atlantis rendezvoused and docked with Mir space station on Nov 15. After departure the Russian-built 316GK Shuttle-Mir docking module remained attached to Mir to provide easier docking capability in the future.

  • 1995 November 20 - Landing of STS-74. 

    STS-74 landed at 17:02 GMT.

  • 1995 December 8 - EVA Mir EO-20-2.  Spacecraft: Mir.

    Repositioned docking adapter.

  • 1995 December 18 - Progress M-30.  Spacecraft: Progress M. Mass: 7,068 kg (15,582 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 20 Dec 1995 16:10:15 GMT. Undocked on 22 Feb 1996 07:30:02 GMT. Destroyed in reentry on 22 Feb 1996 11:02:36 GMT. Total free-flight time 2.22 days. Total docked time 63.64 days.

  • 1996 February 8 - EVA Mir EO-20-3.  Spacecraft: Mir.

    Retrieved and installed material samples

  • 1996 February 21 - Soyuz TM-23.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-21. Soyuz TM-23 docked with Mir at 14:20:35 on February 23.

  • 1996 February 29 - Landing of Soyuz TM-22. 

    Soyuz TM-22 landed at 10:42 GMT.

  • 1996 March 15 - EVA Mir EO-21-1.  Spacecraft: Mir.

    Telescopic boom installed.

  • 1996 March 22 - STS-76.  Spacecraft: Atlantis. Mass: 6,753 kg (14,887 lb). Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Shuttle-Mir Mission 3. Docked with the Mir space station 24 March 1996; Shannon Lucid was left on Mir for an extended stay. First American EVA on Mir. Payloads: SPACEHAB/Mir 03; KidSat; Shuttle Amateur Radio Experiment (SAREX) II, Configuration M; RME 1304—Mir/ Environmental Effects Payload (MEEP); orbiter docking system RME 1315; Trapped Ions in Space Experiment (TRIS); Extravehicular Activity Development Flight Test (EDFT) 04.

  • 1996 March 27 - EVA STS-76-1.  Spacecraft: Mir.

    Attached MEEP materials exposure experiment to outside of Mir (retrieved on STS-86).

  • 1996 March 31 - Landing of STS-76. 

    STS-76 landed at 13:28 GMT with the crew of Chilton, Clifford, Godwin, Searfoss and Sega aboard.

  • 1996 April 2 - Mir News 296: American EVA outside Mir. 

    The EVA made by Clifford and Godwin on 27.03.96 lasted 6 hrs and 2 mins. The Mir crew experienced this EVA passively: their involvement consisted of observing and filming the event through some portholes. It was not easy to cover all activities of the American astronauts fully. They could see a part of the EVA through a porthole in de airlock of Module-D. The best view they got was through the porthole of the cabin of the board engineer in the Base Block. During the EVA the communications went via American channels. On the EVA frequency 279.000 mc Clifford and Godwin could be heard now and then. The same transmissions could be heard via the CNN relay from a TDRS. The Americans installed the experiments on the outer surface of the Docking Compartment at the Kristall-module. (The Russians speak about the 'SO'. The 'O' stands for Otsek, which means 'compartment'. So the do not speak about 'module'.) Atlantis-Mir-combination: During the period in which Atlantis and Mir were linked together many activities took place during the night in our area. We were lucky that this was not so during the EVA, which took place during our morning hours. The operations during the precursor flights cast a gloom over the future. It becomes obvious who will be in command during the flight of the International Space Station: undoubtedly this will be the Americans. Immediately after the docking the Americans took over the attitude control of the whole complex, and most of the communications and the control of the operations were theirs. Undocking of Atlantis. This took place on 29.03.96 at 0108 UTC. After the undocking Atlantis made a flight around the Mir complex and moved away at abt 1 hour later. Onufriyenko could be heard on the Mir-frequencies 130.625 and 143.625mc speaking about the attitude (movements-) control of the Mir station which was now under full control of FCC Kalingrad again. (TsUP-M). The transmissions of the images from Mir about the Atlantis were relayed by tracking stations inside Russian territory.

    Mir: The passes of Mir for our area take place during the night hours and so there is not much to report about the life on board. Module Priroda: The launch of this module has been put back again. Latest available planned launch date: 23.04.1996. Chris v.d. Berg, NL-9165/A-UK3202

  • 1996 April 15 - Mir News 297: Mir. 

    Plans for the near future:

    The first operation will be the launch of the module Priroda. The Russians want to launch this module on 23.04.1996, but further delay might be possible. In fact all is ready for that launch, but specialists responsible for the power supply of that module want to be sure that the accumulators are fully reliable if unexpected the Priroda has to fly longer than the estimated period between launch and docking. The Priroda has not been equipped with solar panels and if the accumulators show failures there are no alternatives. That is why the experts responsible for the power systems and energy consumption take more time for tests. The dates for some important operations can be set only after the launch and successful docking of Priroda and the redocking thereafter. Priroda has to dock to the forward axial port (-X axis) and will be repositioned from there to the radial port (+Z axis). After this the date for the launch of the freighter Progress-M31 can be determined.

    2d Spacewalk (EVA) 21st Main Expedition Mir: Possibly this operation will be executed in May this year. The cosmonauts will have to transfer one of the solar panels which have been brought to Mir by Atlantis (STS-74) and who are still attached at the outer surface of the Docking Compartment (SO - so not Docking Module. SO stands for 'Stykovochnyy Otsek'). They will have to transfer that solar panel to the astrophysical module Kvant-1 (Module-E). During this operation they will use the 2d Strela, which they installed during their first EVA. With this 2d Strela-crane they have the possibility for movements between the SO and the Kvant-1. Originally the Russians planned to install on Kvant-1 the solar panel which is still at the outer surface of the Kristall-module, but they preferred the installation on Kvant-1 of a brand new one. The Russians hope to accomplish this task during that 2nd EVA, but they are ready to insert a 3rd EVA if necessary. The solar panels which have been brought to Mir on the outer surface of the SO will not be deployed from there, but will be used on parts of the Mir-complex.

    VDU: This abbreviation stands for External Engine Installation. This is the box, which can be seen in the top of the long Sofora mast which has been erected on Kvant-1. Nobody was sure about the use or the usefulness of that engine. In an interview Thomas Reiter told me that this VDU often is used for the orientation of the complex during periods in which the gyrodynes have to be silenced for repositioning. These gyrodynes cannot turn through 360 degrees and so now and then repositioning is necessary. There is a problem for the future: when the fuel of the VDU has been spent refuelling will not be possible. Perhaps the Russians hoped that fuel would be sufficient for the VDU at least until the end of the operational life of Mir in 1997 or 1998. So if they want to prolong the use of Mir by some years they will have to find a way to refuel that VDU or to install a new one.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 April 22 - Mir News 298: Launch Priroda. 

    The planned launch date/time for the Module Priroda is 23.04. 1996 at 11hrs 48mins 43secs UTC. If all goes according to plan the Priroda will dock to Mir (forward docking port transition section -P.Kh.O.-, -X axis) on 26.04.1996 at 1203 UTC.

    Priroda: The module for remote sensing Priroda is also known as TsM-I and 77KSI. In space Priroda has a mass of 19.5 tons. The mass of the payload is 10.5 tons, among which 1.2 tons as a supplement for the equipment of the Mir-complex, the remote sensing equipment has a mass of 4.7 tons and Priroda can transport 1.8 tons cargo. The original planning foresaw in a solar array in the front of Priroda (axial), but the place of the array is now used for the installation of extra equipment and experiments. So during the autonomous flight Priroda has to depend on the nickel cadmium accumulators for her power supply. Priroda must have an active lifetime of more than 3 years.

    Cargo: Priroda will also deliver additional equipment to the Mir station, experiments for Shannon Lucid and the SAFEX-2 transceiver for radio-amateur activities.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 April 23 - Priroda.  Spacecraft: Priroda. Mass: 19,000 kg (41,000 lb). Launch Site: Baikonur. Launch Vehicle: Proton.

    LEO. Remote sensing module for Mir space station Docked with Mir Apr 26.

  • 1996 April 24 - Mir News 299: Launch Priroda. 

    The Priroda module blasted off from Baykonur on 23.04.1996 at 11.48.50 UTC, so 7 secs later than planned.

    During the first day the flight went well, all systems functioned normally. On 24.04 two orbit corrections will be executed to bring Priroda in a higher orbit. This will also be done on 25.04. After the corrections on 25.04 the orbit must have an apogee of 404 KM and a perigee of 358 KM. On docking day (26.04) the last 2 orbit corrections will take place.

    Estimated day/time of docking:

    On 26.04.1996 at 12.43.00 UTC. So the soft docking (Kasaniye) will take place just a few minutes after LOS of both objects for our position during the first pass over here in Mir's orbit 58195 and Priroda's orbit 48. So there might be traffic from Mir about the approaching Priroda between 1233-1238 UTC. Undoubtedly the Russians will use the eastern geostationary satellite (Altair-2 on 96 dgs East) for communications, but mostly during such operations traffic can also be monitored on VHF. Possibly it might be worthwhile to monitor Mir/Altair-1 windows in the period before approach and docking.

    Repositioning of Priroda: If the docking on 26.04.1996 will be successful the repositioning of Priroda will take place on the next day, 27.04.1996. Priroda will be repositioned by a manipulator arm (the Lyappa) from the forward port of the transition section (P.Kh.O.), -X axis to the radial port of that section, +Z axis.

    Progress-M31: The launch date of this freighter depends on the docking- and repositioning operations with Priroda. If this all goes according to plan Progress-M31 will be launched on 8.05.1996.

    Safex-2: In fact this complete radio-amateur station has been installed in Priroda and does not belong to the cargo transported by that module. For this radio station 3 antennae have been installed on Priroda.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 April 26 - Mir News 300: Priroda successfully docked with Mir. 

    After an automatic approach guided by the system Kurs Priroda linked up with Mir complex on 26.04.1996 at 1243 UTC. Quite an achievement to aim and dock a mass of 20 tons (like a huge locomotive) with a precision of less than millimetres. Priroda can take a breath for a while at the forward axial docking port of the transition section (P.Kh.O.). During the first pass of both objects for our position in Mir orbit 58195, 1235-1239 UTC, it was obvious that there were no intentions to switch over to the manual remote control TORU. At 123530 UTC Onufriyenko reported that Priroda was hovering for a while in a distance of 182 M and that all was going well. From that distance Priroda started the final stage of the approach and flawlessly docked with Mir. Just like during the whole autonomous flight the Telemetry transmitters of Priroda in het UHF band could be monitored. During the passes after the docking these transmitters remained active. Reason for this is the fact that Priroda will remain electrically autonomous until the accomplishment of the repositioning to the +Z axis.

    On 27.04.1996 at 0800 UTC Priroda will remove itself with a manipulator arm (the Lyappa) to the +Z axis. After that operation the airseal can be checked before the opening of the hatches. The repositioning will take place out of our range.

    A part of the cargo of Priroda consists of biological experiments for the production of clean medical preparations and 900 KG equipment and experiments for the American astronaut Shannon Lucid. Priroda has been equipped by a lot of equipment for scientific research of the earth (all kinds of devices and camera's for remote sensing) and the atmosphere.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 April 30 - Mir News 301: Priroda. 

    On 27.04.96 Priroda has been redocked from the -X to the +Z axis. This operation began at 0830 UTC and lasted app. 2 hours. During the first pass of the complex for our position (orb. 58211, 1310-1319 UTC) the cosmonauts just finished the airseal checks and opened the K.V.D., the valve for the equalisation of the pressure. The cosmonauts also took air samples of the atmosphere inside Priroda for analyses. Just before LOS (Loss of Signal) for our position the hatch to Priroda was opened.

    Power supply problems: Radio traffic during 27, 28 and 29.04.96 revealed that the cosmonauts worked on problems regarding the power supply of Priroda. After the redocking Priroda will get power from the S.E.P. (power supply system) of the Mir complex.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 May 4 - Mir News 302: Progress-M31. 

    The launch of this freighter has been put forward to 5.05.1996 at 0704 UTC. If all goes according to plan the freighter will link up with Mir on 7.04.1996 at 0853 UTC.

    Spacewalk (EVA): It might be possible that the 2d EVA of the crew of the 21st Main Expedition to Mir will be put forward too. The date 8.05 has been mentioned, but the exact date still has to be determined.

    Priroda: The repositioning of this module on 27.04. took place between 0830 and 0920 UTC, so considerably shorter than originally reported.

    SAFEX-2: This radio-amateur station on board Priroda cannot be used before the Priroda is unpacked and fully operational.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 May 5 - Progress M-31.  Spacecraft: Progress M. Mass: 7,140 kg (15,740 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Delivered 1,140 kg of fuel and 1,700 kg of cargo to the Mir complex. Docked with Mir on 7 May 1996 08:54:19 GMT. Undocked on 1 Aug 1996 16:44:54 GMT. Destroyed in reentry over the Pacific on 1 Aug 1996 20:33:03 GMT. Total free-flight time 2.23 days. Total docked time 86.33 days.

  • 1996 May 7 - Mir News 303: Launch Progress-M31. 

    The freighter Progress-M31 was launched from Baykonur on 5.05.96 at 07.04.18 UTC. During the following passes within our range the TLM and Bcn transmitters on 166, 165 and 922 mc could be monitored.

    On the 2d day of the flight again signals from Progress-M31's transmitters.

    Docking Progress-M31: On 7.05.1996 at 08.54.17 UTC Progress-31M docked automatically at the forward axial docking port of the Mir-complex (-X axis). During the first pass over here of both objects in orb. 58364 (1016-1026 UTC) Onufriyenko could be heard reporting data of the approach. He was following the approach on the screen of the TORU (remote guidance from the inside of Mir) monitor. He was ready to take over the guidance if necessary or ordered by TsUP. On the screen he could see the docking port where Progress-M31 had to dock.

    Opening of the hatch: Already during the next pass in orb. 58365 they accomplished the airseal checks and opened the hatch at 10.25.11 UTC, so within our range.

    Cargo: This has a mass of 2410 KG and consists of the normal cargo delivered by Progresses: water, fuel, letters, equipment, repair material etc.

    Spacewalk (EVA): The next EVA of this crew is on schedule for 18 or 19.05.1996.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 May 17 - Mir News 304: 2d Spacewalk (EVA) crew Mir's 21 Main Expedition. 

    This EVA will be the 1st of a series of 3, still to be done by this crew. The EVA will begin on 20.05.1996 at 2255 UTC (opening of the hatch) and end on 21.05.1996 at abt. 0400 UTC (closing of the hatch). During this EVA a solar panel will be transferred from the Docking Compartment, DC, to the astrophysical module Kvant-1 (Module-E). This solar panel had been delivered together with that DC by Atlantis in November 1995. The cosmonauts Onufriyenko and Usachov will transport themselves and the solar panel using the 2d Strela girder, which they installed on Kvant-1 during their first EVA on 15.05.96. The solar panel is folded up and will only be installed on Kvant-1. The deployment and tests will take place during the next EVA. During passes in which the EVA might still be going on EVA-traffic can be monitored on 143.618 and 130.165 mc. (21.05.96 from 0340-0349 UTC and possibly during pressure equalisation of the airlock between 0515-0525 UTC).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 May 21 - EVA Mir EO-21-2.  Spacecraft: Mir.

    Installed MCSA solar array.

  • 1996 May 21 - Mir News 305: 2d Spacewalk (EVA) crew 21st Main Expedition to MI. 

    The EVA began on 20.05.96 at 2250 UTC (opening hatch) and ended on 21.05.96 at 0410 UTC (so duration 5 hrs 20 mins.). During the EVA all went well and that what the crew had to do has been accomplished for 100% . The crew transferred a solar battery from the outside of the docking compartment (SO) to the Kvant-1 (Module-E). For their work the cosmonauts used the 2d Strela girder.

    Radio traffic between the cosmonauts and Sannon Lucid who kept watch on board Mir went via the normal VHF-frequencies and was relayed via the geostationary satellite Altair (Kosmos-2054) on 16 dgs West. Shannon assisted the cosmonauts during the putting on and off of their spacesuits. During the EVA she took care for the systems of the space station and the communications.

    3d EVA: This is on schedule in the night from 24 to 25.05.96. Opening of the hatch on 24.05 at 2050 UTC, closing of the hatch on 25.05.96 at 0205 UTC. During this EVA the cosmonauts will deploy, connect and test the solar panel on Kvant-1.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1996 May 25 - EVA Mir EO-21-3.  Spacecraft: Mir.

    Deployed MCSA solar array.

  • 1996 May 25 - Mir News 306: 3d Spacewalk (EVA) crew 21st Main Expedition Mir. 

    The cosmonauts Onufriyenko and Usachov made this EVA between 24.05 at 2047 UTC and 25.05 at 0230 UTC. This EVA lasted somewhat longer than planned, but all went well. The cosmonauts installed the new solar panel on the outer surface of Kvant-1, connected the contacts and attended the deployment of that panel. This was also a good performance. During the last phase of the EVA radio traffic went via Altair-1 (Cosmos-2054) and the known VHF-frequencies. After returning inside Mir the cosmonauts expressed their satisfaction about the good co-operation with TsUP during this work and also about the very good construction of the new solar panel.

    4th EVA: This EVA is on schedule for 30.05.1996 between 1900-2100 UTC. Main task will be the transfer of the MOMS (opto-electronic stereo scanner) to the outer surface of the Priroda module and the installation of this device over there. The MOMS has been delivered to Mir as a part of the cargo of the Priroda. Apart from this work they will also have to accomplish some minor tasks.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 May 30 - EVA Mir EO-21-4.  Spacecraft: Mir.

    Multi-Spectral Scanner installed.

  • 1996 May 31 - Mir News 307: 4th Spacewalk (EVA) Onufriyenko and Usachov. 

    This EVA started on 30.05 at 1820 UTC (opening of the hatch) and ended on 30.05. at 2240 UTC (closing of the hatch). The MOMS-2 camera (Modular Opto-electronic Multi-spectral/ Stereo scanner has been installed on the outer surface of the module Priroda. The 2d task was the installation of an extra handrail outside Priroda to facilitate EVA's. The EVA passed without problems.

  • 1996 June 5 - Mir News 308: 5th Spacewalk (EVA) Onufriyenko and Usachov. 

    This EVA is planned for 6.06.1996 between 1655 UTC (opening hatch) and 1930 UTC (closing hatch). During this EVA the cosmonauts will work at the outer surface of module Spektr and module Kvant-2 ('D'). On Spektr they will replace the cassette of the Komza-experiment. Then they will retrieve some American and Russian dust collectors from Module Kvant-2 ('D').

    6th EVA Onufriyenko and Usachov:

    This EVA will take place on 13.06.1996. Times not decided yet. During this EVA the cosmonauts will install Ferma-3 (a girder or truss construction) at the outer surface of the astrophysical module Kvant-1. Experience with constructions like these are very important for the future. They will be used for the building and exploitation of the International Space Station Alpha.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 June 6 - EVA Mir EO-21-5.  Spacecraft: Mir.

    Retrieved and installed material samples

  • 1996 June 7 - Mir News 309: 5th Spacewalk (EVA) Mir-crew. 

    This EVA took place on 6.06.1996 between 1656 UTC (opening of the hatch) and 2030 UTC (closing of the hatch). At the outer surface of the Module Spektr they replaced a cassette of the KOMZA-experiment (a Swiss experiment for the study of inert interstellar gasses) and at the outside of Module-D (Kvant-2) they installed some detectors for space dust and space debris: an American instrument and the SKK-11, a Russian made device. The EVA lasted 1 hour longer than had been planned. Onufriyenko and Usachov needed for their work and movements considerably more time than had been foreseen in the so called cyclogram for this EVA. During the EVA communications took also place via the geostationary satellite Altair-1 (Cosmos-2054). Now and then the EVA cosmonauts gave instructions to Shannon Lucid who was on duty inside the complex and observed the EVA through portholes.

    6th EVA: Still on schedule for 13.06.96. Times not yet decided. Task: Installation of the Ferma-3 girder construction at the outer surface of the astrophysical module Kvant-1.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 June 13 - EVA Mir EO-21-6.  Spacecraft: Mir.

    Assembled truss. Deployed SAR radar antenna.

  • 1996 June 13 - Mir News 310: 6th Spacewalk (EVA) Mir-crew. 

    This EVA began earlier than planned on 13.06.96 at 1245 UTC (opening of the hatch) and lasted until 1827 UTC (closing of the hatch). They had to accomplish some very strenuous tasks: the installation and deployment of the Ferma-3 girder construction at the outer surface of the Kvant-1 module and the repair of the Travers-antenna (the huge SAR antenna on the module Priroda). They deployed the 4 sections of the Ferma-structure until the desired length of 5 meters. The Travers radio locator antenna had not been fully deployed by commands from inside the module Priroda and so Onufriyenko and Usachov completed this manually during their EVA. The Travers is now operational. After this work they made their way back to the airlock of Module-D. This was not easy and went slowly. (It is the last straw that can brake the camel's back). Back on board the cosmonauts quickly recovered and expressed their satisfaction about the accomplished tasks but also about the assistance they got from Shannon Lucid being on command inside the complex. She had been busy with camerawork and used all available films and cassettes. TsUP also thanked her for her work during the EVA. This has been the last EVA planned for this crew. The next EVA has to be made by the next crew in September this year.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 4 - Mir News 311: Progress-M32. 

    The launch of this freighter has been put back again and is now on schedule for 22.07.1996. The Progress-M32 has to deliver new supplies of water, fuel, oxygen, food, etc. to the Mir-space station. The reason for this delay are two failures with the Soyuz-U rocket, which also is used for the launches of Progress-M ships.

    Soyuz-U: Within the period of some weeks 2 launches of reconnaissance satellites with the carrier Soyuz-U failed. The first time this was on Baykonur on 13.05. 49 seconds after lift off the payload fairing came loose and the control-system gave the command for self-destruction. The commission to investigate the accident failed to find a unanimous conclusion. 4 different possibilities had been suggested even the rather bizarre idea that a big bird collided with the rocket. Normally all launches of analogue rockets are suspended until the experts know for sure the cause of the accident. This time they did not wait until a definite conclusion and launched another spy-satellite, now from Plesetsk using the rocket Soyuz-U. And again exactly after 49 seconds the fairing came loose and rocket and satellite were destroyed. This time the commission started a thorough investigation, which is still going on. So possibly the launch of the freighter Progress-M32 will be put back again.

    Mir-routine: Life goes on: the 2 Russians and Shannon Lucid are still in a very good mood. They do not seem to worry about the 'rocket' problems. The relief crew for Onufriyenko and Usachov has to fly with the Soyuz-TM24 on 14.08.1996. This crew consists of the Russians Manakov and Vinogradov and de French cosmonaut Claudie Andree-Deshays. For this launch a modified rocket, the Soyuz-U2 is needed. Financial problems might put a spoke in the wheel. During the last week Shannon Lucid worked with the Glove box. She met some problems with contacts and switches but resolved these by the help of an expert at TsUP Moscow. Shannon Lucid will be relieved by John Blaha during the 4th Shuttle-Mir docking mission STS-79 by Atlantis in the beginning of August.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 9 - Mir News 312: POSSIBLE CHANGES IN PLANNING NEAR FUTURE. 

    During the launch of Columbia on 20.06.1996 hot gasses leaked through the insulation of the rocket boosters. This might cause a month's delay in the launch of Atlantis -STS-79- 4th docking mission with Mir. During radio traffic from Mir Shannon Lucid confirmed that she takes into account the possibility that she might return in the first week of September. During the mission of Atlantis Lucid has to be relieved by John Blaha.

    Soyuz-TM24: Shannon Lucid also said that the Russians still stick to the launch of this ship on 14.08.1996 with Manakov, Vinogradov and Claudie Andree-Deshays and the return of Onufriyenko and Usachov together with the French guest-cosmonaut on 30.08.1996 with the Soyuz-TM23. So possibly Lucid will be in the Mir-station during the mission of Andree-Deshays.

    Progress-M32: If there will be permission for the use of the rocket Soyuz-U before 21.07.1996 this freighter will be launched from Baykonur in the night from 21 to 22.07.1996.

    Just before the deadline for this report the press-service of TsUP near Moscow did not have information about changes and sticks to the original schedule: Launch Atlantis: 31.07.1996, Launch Progress-M22: night from 21. to 22. 07.1996, and Launch Soyuz-TM24: 14.08.1996.

    Moscow confirmed that changes might be possible.

    Chris van den Berg, NL-9165/A-UK3202

  • 1996 July 14 - Mir News 313: Atlantis - STS-79 4th Mir Docking mission.. 

    On 11.07.96 the NASA decided to take a decision about the flight of Atlantis next week, but already within 24 hours NASA decided to postpone the launch of Atlantis until the midst of September. For that flight Atlantis will be equipped by the boosters used before the use of the modified boosters which have been used during the launch of Columbia on 20.06.96. So Shannon Lucid will have to stay on board of the Mir-station 1.5 month longer. She will be there during the mission of the French cosmonaut Claudie Andree-Deshays (Cassiopea) and for a while working under command of Manakov.

    Progress-M32: Still to be launched in the night from 21 to 22.07.96.

    Soyuz-TM24: The ship will have to bring the relief crew and the French cosmonaut to the Mir-station. Soyuz-TM24 with a crew of 3 persons will be launched by the use of the rocket Soyuz-U, so not with the more powerful Soyuz-U2. To enable Soyuz-TM24 to have a rendezvous with Mir after being launched with a Soyuz-U rocket , the Mir-station had to be brought in a lower orbit. The engines of the Progress-M31 corrected Mir's orbit on 2 and 4.07.96.

    Radio-amateur traffic: Now and then phone from Mir on 145.550 mc. That what is needed for Packet radio traffic is always in use for service traffic on 143.625 mc. The downlink signals of the Mir-station only give the P/R confirmation (R0Mir-CUP). The transmitter of Safex-2 in the Priroda-module can be heard in a recorded greeting in Russian and English on 437.925 mc, FM-N. This frequency is also in use as a primary frequency for ISM-purposes (Industrial Scientific and Medical), which means that there might be a lot of interference if that frequency is in use for ISM by local stations, for instance hospitals.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 16 - Mir News 314: Progress-M32. 

    The launch of this freighter with new supplies for the Mir-space station is on schedule for 21.07.1996 at 23.58.06 UTC (For Moscow summertime already on 22.07.96). So for the launch of this freighter green light has been given for the use of the carrier Soyuz-U. (For details about the Soyuz-U problems see MirNEWS.311)

    Soyuz-TM24: The intention still exists to launch this ship with the crew of the 22d Main expedition to Mir (Manakov and Vinogradov) and the French cosmonaut Claudie Andre- Deshays on 14.08.1996, but a final decision has not yet been made. It might be possible that the Russians entrust the launch of the unmanned Progress-M to the carrier Soyuz-U, but wait with the green light for the use of that carrier for a manned ship until the eventual successful launch of the freighter.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 19 - Mir News 315: Progress-M32. 

    The launch of this freighter has been put back again. Using the carrier Soyuz-U Progress-M32 will start from Baykonur on 24.07.1996 at 2347 UTC (Moscow time 25.07.1996 - 0247 UTC)

    Progress-M32 has to link up with Mir at the forward axial port (-X axis). The first approach will be in the automatic mode by the system Kurs. The crew has to be ready to use the TORU (Tele-operating Guidance regime). If the automatic approach will fail the first time the crew will control the approach the next day using TORU. During the pass in orbit 59500 from 0918-0930 UTC today the crew got instructions about this operation.

    During the flight signals from Progress-M32 can be monitored in the 166, 165 and 922 MC bands.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 22 - Mir News 316: CORRECTION. 

    Ref. MirNWS.315: The planned launch time of Progress-M32 is on 24.07.1996 at 2247 UTC. The time in Moscow Summertime is 25.07.1996 at 0247.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 25 - Mir News 317: Progress-M32. 

    The launch of this freighter has been postponed. A few seconds before blast off the control system discovered an irregularity in one of the systems of the carrier Soyuz-U and stopped the operation. An inquiry into the cause of the failure is going on. Depending on this inquiry the decision for the second launch attempt will be made.

    Towards the planned launch time (24.07 at abt. 2247 UTC) the Mir station was in visual range of Baykonur and the crew hoped to see the start. So they did not see anything and during the pass in orbit 59591 (0500-0512 UTC) Onufriyenko asked TsUP why the launch has been postponed.

    Meanwhile the cosmonauts continue the preparations for the departure of the freighter Progress-M31, still docked to the station. They are loading the Progress-M31 with things they do not longer need . Progress-M31 remains docked at the station until the 2d day of the flight of Progress-M32 when it is obvious that the systems of that freighter are functioning normally.

    Soyuz-TM24: About this ship with the relief crew Manakov and Vinogradov and the French spacionaute Claudie Andre-Deshays there will be a press-conference in Ts.P.K. (Starcity) on 26.07.1996. Undoubtedly the failure of the Soyuz-U rocket will be discussed there and we hope to get information about the eventual launch of Soyuz-TM24 on 14.08.1996.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 30 - Mir News 318: Progress-M32. 

    The launch of this freighter is now on schedule for 31.07.1996 at 20.00.04 UTC (For Moscow summertime 4 seconds after midnight on 1.08.96). The decision to give the green light for this launch has been taken on 29.07.1996 during a meeting of the state committee. The first attempt to launch the Progress-M32 failed due to a tank pressurisation problem. During the inspection afterwards a problem was revealed in one of the engines of a booster. The possibility to change that engine has been considered but finally the decision was taken to replace the whole booster. If all goes according to plan we might be able to hear the signals of the beacon- and telemetry transmitters of Progress-M32 at abt. 3 hrs after launch in the 922, 166 and 165 mc bands.

    The estimated docking time of Progress-M32 at Mir: 2.08.1996 at abt. 2159 UTC.

    Soyuz-TM24: The launch of this ship with the relief crew and the French spacionaute is now on schedule for 20.08.1996. We hope to get an eventual confirmation or additional information by CNES during this week.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 July 31 - Progress M-32.  Spacecraft: Progress M. Mass: 7,130 kg (15,710 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. This was the first successful launch of a Soyuz-U after two failures. Docked with Mir at the forward docking port on 2 Aug 1996 22:03:40 GMT. Undocked on 18 Aug 1996 09:33:45 GMT in order to free up the docking port. By 29 August 1994 Mir was in a 375 x 390 km x 51.6 deg orbit; the Progress M-32 cargo ship, flying separately, was in a 375 x 392 km x 51.6 deg orbit. Redocked with Mir on 3 Sep 1996 09:35:00 GMT at the rear port of the Kvant module. Finally undocked from Mir on 20 Nov 1996 19:51:20 GMT. Destroyed in reentry on 20 Nov 1996 22:42:25 GMT. Total free-flight time 2.20 days. Total docked time 93.91 days.

  • 1996 August 1 - Mir News 319: Progress-M32. 

    This freighter was launched from Baykonur on 31.07.1996 at 20.00.06 UTC. All went well and during passes within our range the signals of the beacon- and telemetry transmitters in the 166, 165 and 922.755mc could be monitored. During the pass in orbit 4, 020700-021220 UTC TCA (Time Closest Approach) for the Hague was 020808 UTC (922.755 mc Doppler dip).

    If all continues to go according to plan the Progress-M32 will link up with Mir on 2.08.1996 at 2158 UTC. The first pass (of that sequence) of Mir and Progress-M32 in Mir's orbit 59727, will last from 2147 until 2154 UTC. So during this pass the final approach is going on and radio communications regarding this operation possibly can be monitored in the VHF-band.

    The Progress-M32 will deliver to the Mir-station a cargo of 2478 KG. 328 KG of this cargo consists of experiments and equipment to be used by the French spacionaute Claudie Andre-Deshays during her Cassiopeia mission to Mir this month. The cargo further consists of water, food, fuel, oxygen, letters, equipment, software, spare parts etc.

    Progress-M31: This freighter is still docked at the forward (-X axis) port of the Mir-station and this port has to be free for the arrival of Progress-M31's successor Progress-M32. For that reason Progress-M31 will separate from Mir on 1.08.1996 at 1642 UTC and after a short autonomous flight this freighter will be put on a destruction course and burn up in the atmosphere over a designated area of the Pacific East of New-Zealand.

    Chris v.d. Berg, NL-9165/A-UK-3202.

  • 1996 August 3 - Mir News 320: Progress-M32. 

    Docking at Mir:

    Progress-M32 docked at the Mir-station (-X axis, forward port transition section) on 2.08.1996 at 22.03.44 UTC. So 6 minutes later than planned. Approach and docking were executed in the automatic mode by the use of the system Kurs.

    Radio traffic: As always during such operations the radio traffic was very interesting. During the pass in orb. 59727, 2149-2156 UTC , the approach was still going on. The crew just accomplished a test of the TORU-system (for eventual manual guidance by the Mir-crew). They did not use this system. At 215520 UTC the distance between Progress-M32 and Mir was 180 M. The cosmonauts monitored the images made from Progress-M32 of the station on their displays. They also observed the approaching Progress-M32 via illuminators. The traffic revealed that, though somewhat slower than planned, the operation was proceeding well. During the next pass in orb. 59728, 2327-2333 UTC, radio traffic revealed that Progress-M32 had docked at Mir. The preparations for the opening of the hatches were going on, i.e. airseal checks, the equalisation of the pressures in Progress-M32 and Mir, deployment of an air hose, and so on. During the pass in orb. 59729, on 3.08.1996 from 0057-0107 UTC, the hatches were open and de cosmonauts already had entered the freighter to remove things which had to be transferred to the complex as soon as possible. After checks of the systems of Progress-M32 and the work to be sure that Progress-M32 was fixed at the station tight and safely the crew could go asleep. And so did, tired but satisfied, your 'observer'.

    The Progress-M32, will -relatively- remain a part of the Mir-complex for a short period: If the operations with Soyuz-TM24 (relief crew) will proceed according to plan (of this moment) Progress-M32 has to depart on 20.08.1996 to free the forward docking port for the Soyuz-TM24, which has to be launched on 19.08.1996. Progress-M31: This old freighter separated from Mir on 1.08.1996 at 16.44.54 UTC. and burnt up in the atmosphere. (Further details in a next Mir-report.)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 August 13 - Mir News 321: 22d Main Expedition to Mir. 

    Due to serious hearth rhythm problems Manakov, the commander of the main crew, had to be hospitalised. So the core crew has been replaced by the stand ins. The French spacionaute Claudie Andre-Deshays will stay in the main crew. The crew of the 22d ME will consist of: Valeriy Grigoryevich Korzun (Commander), Aleksandr Yuryevich Kaleri (board engineer) and Claudie Andre-Deshays, (cosmonaut-researcher, guest cosmonaut CNES. ) Vinogradov and Leopold Eyharts remain available for the eventual replacement of respectively Kaleri and/or Andre-Deshays. There is no reserve commander available.

    Launch of Soyuz-TM24: The launch of this ship with the above mentioned crew members has been put forward and will now take place from Baykonur on 17.08.1996 at abt 1317 UTC.

    The service call sign of the crew is FREGAT, so resp. Fregat-1. -2 and -3).

    The names of the new crew and the earlier launch date had been given by a recorded message of Shannon Lucid transmitted from Mir on 437.925 mc.

    Progress-M31: As already has been reported this freighter ceased her existence on 1.08.1996. The exact times of this operation were: Separation from Mir: 16.44.45 UTC, start reentry burn: 19.44.30 UTC and burning up over a designated area in the Pacific East of New Zealand: 2033 UTC.

    Progress-M32: This freighter is still docked at Mir. If the launch and first part of the flight of Soyuz-TM24 will proceed as planned Progress-32 will undock from Mir on 18.08.1996 and burn up in the atmosphere.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 August 16 - Mir News 322: Soyuz-TM24. 

    The most recent information from Moscow confirms that the launch of this ship with the relief-crew for the 22d Main Expedition to Mir is still planned for 17.08.1996 at 1317 UTC. If all goes according to plan Soyuz-TM24 will dock at Mir on 19.08.1996 at 1449 UTC.

    Progress-M32: This freighter will separate from Mir on 18.08.1996 at 0931 UTC. In contradiction to the supposition in MirNEWS.321 Progress-M32 will not be brought on a destruction course, but stay in orbit in an autonomous flight. The Progress-M32 will redock to Mir after the departure of Soyuz-TM23 with the relieved crew. The redocking has to take place on 3.09.1996. Progress-M32 will be used to reboost the Mir-complex in the original somewhat higher orbit after the return to earth of Atlantis (STS-79) in September.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 August 17 - Soyuz TM-24.  Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-22. Valeriy Korzun and Aleksandr Kaleri of the Russian Space Agency (RKA) Claudie Andre-Deshays of the French space agency CNES. This launch was the first of the Soyuz-U booster with a crew aboard following two launch failures of on unmanned flights. Soyuz docked with Mir's front port at 14:50:21 GMT on August 19; Mir was in a 375 x 390 km x 51.6 deg orbit.

    On Feb 7 at 16:28:01 GMT the EO-22 crew and American astronaut Linenger undocked the Soyuz TM-24 ferry from the front docking port, flew it around to the far side of the complex and redocked at the rear Kvant port at 16:51:27 GMT. This cleared the forward port for the arrival of the EO-23 crew, who brought with them German astronaut Reinhold Ewald on Feb 12.

  • 1996 August 18 - Mir News 323: Soyuz-TM24 successfully launched for flight to Mir. 

    The Soyuz-TM24 has been launched with the carrier Soyuz-U from Baykonur on 17.08.1996 at 13.18.03 UTC. Soyuz-TM24 reached the planned orbit without problems and all systems worked well. Already during the pass in the 2d orbit the ship came in our range (1620-1623 UTC) and radio signals could be monitored. Korzun, commander of this 22 Main Expedition, who makes his first flight, reported that they had moved from the SA (landing-apparatus) into the BO (life compartment) and that they had put off their spacesuits. The crew made preparations for the 1st orbit correction which was planned for 16.57.43 UTC. During the pass in the 3d orb. (1749-1756 UTC) the 2d orbit correction was accomplished: 175021 UTC. Korzun reported the good performance of these operations during this pass. During the 4th orbit (1923-1930 UTC) again a lot of radio traffic. 2 times the TCA's (Time Closest Approach) could be determined monitoring the Doppler shift on 922.755 mc: 3d orb. at 175222 UTC and 4th orb. 192520 UTC. In the morning of 18.08.1996 Flight control confirmed that all crew members were in a good health and mood. Due to the use of the carrier Soyuz-U instead of the more powerful Soyuz-U2 the Russians had to reduce the mass of crew and material. So they refrained from the use of Kurs, the device for automatic approach and docking. This means that Korzun will have to approach and dock in the manual mode. The docking is on schedule for 19.09.1996 at 1449 UTC. During the final phase of the docking operation both objects are within our range. (Mir's orb. 59981, 1437-1443 UTC) and radio traffic about this operation might be possible on the Mir and Soyuz-TM24 frequencies.

    Progress-M32: This freighter separated from Mir on 18.08.1996 at 0934 UTC. The autonomous flight of the Progress-M32 will last until 3.09.1996.

    Soyuz-TM23: Return to earth of relieved crew of ME 21 (Onufriyenko and Usachov) and Claudie Andre-Deshays with the Soyuz-TM23 has been put back until 2.09.1996.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 August 19 - Mir News 324: Soyuz-TM24 docked at Mir. 

    The Soyuz-TM24 docked at Mir on 19.08.1996 at 14.50.21 UTC. Approach and docking took place in the automatic mode with the system Kurs. This in contradiction to the information about Kurs in MirNEWS.323. This information came from a usually reliable source who possibly misinterpreted a message of a press-agency. Radio traffic during the passes after the successful docking revealed that the new crew and Claudie Andre-Deshays still were in good health and mood after the 2-days flight. A very cheerful Claudie told a countryman at TsUP that she will use the module Priroda as her guest-room. Shannon Lucid is staying in the module Spektr.

    Soyuz-TM23: This ship will return to earth on 2.09.1996 with the relieved crew of ME 21 and Claudie.

    Progress-M32: This freighter is flying in a somewhat higher orbit than Mir. Progress-M32 will redock at Mir on 3.09.1996.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 September 2 - Mir News 325: Soyuz-TM23 returned to earth. 

    The descent module of the ship Soyuz-TM23 with on board the crew of the 21st ME and the 'spacionaute' Claudie Andre-Deshays landed safely on 2.09.1996 at 07.41.40 UTC in a position 105 KM South West of Akmola in Kazakhstan. The condition of the 3 cosmonauts was excellent and they will fly to Chkalovo (near Starcity, Moscow) today.

    0110 UTC: The hatch behind the departing cosmonauts was closed.

    0417 UTC: Soyuz-TM23 separated from Mir to begin a short autonomous flight.

    The aimed landing position was in a distance of 107 KM from Tselinograd in Kazakhstan with an estimated landing time of 07.41.03 UTC. (So they landed 37 sec. later in another position).

    Progress-M32: This freighter is still flying autonomously. Redocking to the Mir complex is on schedule for 3.09.1996 at abt. 0755 UTC.

    Chris v.d. Berg, NL-9165/A-UK320.

  • 1996 September 2 - Landing of Soyuz TM-23. 

    The spacecraft undocked on September 2 at 04:20 GMT, and made a small seperation burn at 04:24:40 GMT. Deorbit was at 06:47:20 GMT. The three modules separated at 07:14:36 and the parachute deployed at 07:26 GMT. The landing was at 07:41:40 GMT, 100 km SW of Akmola in Kazakstan with Yuri Onufrienko, Yuriy Usachyov and Claudie Andre-Deshays aboard. This concluded the French 'Cassiopee' mission.

  • 1996 September 3 - Mir News 326: Progress-M32 redocked at the Mir space station.. 

    Today Progress-M32 concluded her autonomous flight. This flight began on 18.08.1996 , so 1 day before the docking of Soyuz-TM24. Approach and docking took place 1 orbit later than originally planned and was executed in the automatic mode with the system Kurs. The docking at the aft docking port (Kvant, +X-axis) was accomplished on 3.09 at 09.35.21 UTC. For those monitoring operations like this the delay of this operation until orbit 60212 from 0927-0932 UTC was a piece of good luck because of the fact that they could monitor the final phase of the operation. Commander Korzun observed the approach via the displays of the systems LIV and TORU and reported distances, approach speeds and manoeuvres around the X-axis. When both objects disappeared behind the horizon the distance was 95 meters and the appr. speed 0.8 M/sec. During the pass in orb. 60213 from 1102-1108 UTC it was obvious that Progress-M32 was a part of the Mir-complex again. Meanwhile Korzun had corrected the attitude of the complex. He got orders not to carry out the airseal checks and the opening of the hatch today.

    (So in a relative short period the Russians successfully accomplished crucial operations. As far as Russian spaceflight is concerned Aleksandr Lebedj has nothing to worry about!!)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 September 12 - Mir News 327: Activities on board Mir. 

    The crew has spend a lot of time and efforts to repair an airseal problem in one of the modules. Obviously the problem has been solved, but the cause of that what might have been a leakage seems to be a mystery. Meanwhile the crew started preparations for the meeting with the Atlantis (STS-79) still to be launched on 16.09.1996 at 0854 UTC. Apart from extra physical training Sannon is packing things which she has to transfer to Atlantis for delivery on earth. Assisted by Kaleri, who also gave her instructions, Shannon tried out a spacesuit. She reported (in Russian) to TsUP that the suit was the right size and that she was sure to be able to use it if this might be unlooked-for necessary. TsUP confirmed that this exercise had to be done in case of an eventual return of Shannon with a Soyuz-TM. One of the means to inject oxygen in the atmosphere of the complex is the system Elektron. These systems produce oxygen out of water by an electrolysis process. Nitrogen is needed for the purging of these Elektrons, but also for the pressurising. Nowadays there is not enough nitrogen on board and new supplies, which have to be delivered by Atlantis and Progress-M33 (in October) are badly needed.

    Atlantis (STS-79): If all goes according to plan and Atlantis starts on 16.09.1996 at 0854 UTC radio-amateurs in Western-Europa can try to monitor phone reports from Atlantis at abt. 20 minutes after launch. This might be possible during the first contact of Atlantis via a relay-facility in Spain. During the last flight of Atlantis signals could be monitored on 259.700 mc AM. After an elapsed time of 2days 18hrs 23mins Atlantis must link up with Mir, so if the launch goes as planned and the flight has been proceeding well this will take place on 19.09.1996 at 0017 UTC (for the USA still 18.09). If the same communications are used as during the last Atlantis mission an American TDRS as well as a Russian Altair (1 or 2 or both) will be used during approach and docking. 23 minutes after the 'soft docking' the so called 'hardmate' will take place. After a check period of 2hrs and 25mins the hatches will be opened.

    Radio-amateurism: During the last week a lot of traffic, Packet Radio and Phone could be heard on 145.550mc. Korzun is an enthusiast radio-amateur and he made a lot of QSO-s over Western Europe. His knowledge of the English language and his feeling for radio-amateurism enables him to do this and to enjoy it. Apart from some recorded voice messages on 437.925mc I cannot say much about the use of the Safex-2 facilities in the Priroda module. Here the UHF-frequencies 437.925, 437.950 and 437.975 mc are used for medical purposes (hearth monitoring) by a hospital nearby. Monitoring these frequencies is such a torment that it would endanger the condition of my hearth in such a way that I myself even might need that service by that hospital!

    Chris van den Berg, NL-9165/A-UK3202.

  • 1996 September 16 - Spacehab Double Module.  Spacecraft: Spacehab. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Remained attached to OV-104

  • 1996 September 16 - STS-79.  Spacecraft: Atlantis. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    On September 19 Atlantis docked with the Russian Mir space station. Aboard Atlantis in the payload bay were the Orbiter Docking System, the modified Long Tunnel, and the Spacehab Double Module, containing supplies for the Mir. Astronaut John Blaha relieved Shannon Lucid as NASA resident on the complex. Atlantis undocked from the Mir complex on September 23 at 23:33 GMT. Valeriy Korzun, Aleksandr Kaleri and John Blaha remain on Mir. On September 26 Atlantis closed its payload bay doors, and at 11:06 GMT fired its OMS engines for a three minute long deorbit burn. After entry interface at 11:42 GMT the spaceship flew across Canada and the US for a landing at the Kennedy Space Center's Runway 15 at 12:13 GMT.

  • 1996 September 17 - Mir News 328: Start Atlantis. 

    Within 20 minutes after the launch of Atlantis on mission STS-79 on 16.09.1996 at 08.54.49 UTC commander Readdy could be heard in a contact with Houston via a relay station in Spain. This was on 259.700 mc (AM) between 0913-0919 UTC. For ballistic reasons lift-off took place 46 seconds later than originally planned.

    Rendezvous and docking operations:

    Begin Mir rendezvous operation: 18.09 2134 UTC TI Burn 19.09 0003 Arrival on R-bar (Earth radius vector) 0153 Hovering at 170 feet from Mir 0235 Begin final approach 0310 Atlantis docks with Mir 0317 Hardmate Atlantis/Mir 0337

    For observers in Western-Europe the passes of Mir (and -the then being in a short distance- of Atlantis) begin during Mir's orbit nr. 60468 with a pass between 0307-0315 UTC, maximum elevation 11 degrees. So communications between Mir and Atlantis might be possible on the well known VHF frequencies. Whether there will be TV-images -for instance via CNN- or not is not sure at this point. If the Russians use Altair-1 (Cosmos-2054) over 16 dgs West images seen by Mir of the approaching Atlantis might be possible between 0230-0324 UTC. During the last docking mission of Atlantis (STS-76) those images could be seen via CNN together with images of Mir seen by a camera in Atlantis. It is also possible that the Russians will use Altair-2 (over 96 dgs East) during the window from 0306-0402 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1996 September 19 - Mir News 329: Atlantis docked at Mir. 

    'Readdy was ready' and he controlled the free drift with a speed of appr. 2.5 cm/sec of Atlantis to Mir during the final phase of the approach. The result was a perfect soft docking on 19.09.96 at 0313 UTC. The original operation schedule was almost executed on the minute, except for the time of the 'touch', which had been put forward by 4 minutes. For friends in Western Europa who use to monitor radio transmissions during such operations this was a blessing for it meant that the docking could take place within the window for both objects on Mir's orbit nr. 60468, 0307-0315 UTC. So at 031330 UTC they could hear Readdy reporting in Russian: 'KASANIYE' (touch). For this report he used the 130.165 mc FM and immediately after his report commander Korzun in Mir reported on 143.625 mc that he had a positive indication about the docking. Monitoring people always hope that they can pick up that important word 'kasaniye' during dockings of Soyuz- and Progress-ships, but mostly the moment of that touch takes place just a few minutes after LOS of their position, in the past this occurred a few times during Soyuz-TM dockings. Of course it is always possible to log the traffic during such dockings in the final phase of the approach. This time there was not much radio traffic before the 'touch' for Readdy had to do his job with concentration and everybody was watching the operation silently. TV-images transmitted by TV-stations revealed that there were no direct images from camera's on board Mir. So possibly the geostationary Luches: Altair-1 and 2 were not in use. During the first 3 docking missions these images could be seen simultaneously with the images from Atlantis , relayed by TDRS-s. Certainly we will get images made from inside Mir during the docking operation, but these were recorded and transmitted to earth later. During the next pass of the enormous space-complex (in orb. Mir nr. 60469, 0441-0453 UTC) the Mir-crew already had accomplished the air-seal checks and opened 2 hatches of the SO (docking compartment). They also had removed things which had been necessary during the docking and now had to be stowed away. Just before LOS for our position Korzun tried to communicate via 130.165 mc with Atlantis to get information about the proceedings there. Opening of the hatches from Atlantis to Mir took place at 0539 UTC, so not in our VHF-range. Via TV-stations receiving relays via a TDRS we could see nice images of the meeting of both crews and the first gathering on board Mir.

    SAREX STS-79: During this mission there might be radio-amateur activities by the astronauts-radio-amateurs Jay Apt (N5QWL), Carl Walz (KC5TIE) and John Blaha (KC5TZQ). Sarex VHF downlink is 145.840 mc FM with uplink frequencies: 144.450 and 144.470 mc FM. Please do not use 145.840 mc FM for 'uplink' or -during Atlantis passes -local bragging. Chris v.d. Berg, NL-9165/A-UK3202

  • 1996 September 26 - Landing of STS-79. 

    STS-79 landed at 12:13 GMT with the crew of Lucid, Readdy, Wilcutt, Akers, Apt and Walz aboard.

  • 1996 October 7 - Mir News 330: Progress-M33. 

    The launch of this freighter was planned for 15.10.1996. Due to problems with the carrier-rocket the launch has been put back possibly to 2.11.1996.

    Mir-routine: Mir's passes for our position are gradually shifting from the night to the late evening hours. So still not much traffic via VHF. Now and then the Russians use the geostationary Altair-1 (Cosmos-2054) for Mir-communications. On 5.10.1996 the crew spoke with TsUP about a lot of condenstation in a cable compartment. Possibly this problem has been resolved as they did not mention it the next day. During conversations with TsUP on 6.10.1996 the cosmonauts mentioned the dismissal of Gen. Ivanov from his command of the VKS (space forces). They supposed that this also means that Gen. Ivanov also has been relieved of his chairmanship of the State Committee for Spaceflight. This committee always selects which crew will fly and the chairman takes the oath of departing crews. General Ivanov has a long and excellent career in spaceflight and the relinquishment of his command must be a heavy blow for Russian spaceflight. At least this is my opinion, but I am sure that the cosmonauts will share this opinion with me. John Blaha: He is like his predecessor very active and from conversations in Russian as well in English with specialists on earth can be derived that he is very enthusiastic. He still has to accustom himself to the differences between his training in replicas on earth and the practice in space. On earth things in training modules have been put straight in contradiction to the situation on board. Often it takes him a long time and consultations with the earth to find things he needs for his experiments. During passes of the Mir-station during working hours it might be possible that Blaha uses the 130.165 mc while his Russian colleagues use 143.625 mc. The arrangement for the use of 130.165 mc will be made on 143.625 mc. They speak about UKW-dva , they mean 130.165 mc.

    Radio-amateur traffic: The 145.550 mc is fully in use for Packet radio and often Korzun can be heard in phone with amateurs on earth. Korzun is a skilled and enthusiastic radio-amateur. It is also worth while to monitor the 437.925 and 437.950 mc for traffic via the Safex installation in the Priroda module. The 437 mc band is primary for ISM-purposes (Industrial, Scientific and Medical). In my neighbourhood this band is fully blocked by a hospital using that band for health monitoring equipment. I would be very pleased to hear experiences in this field from friends in other parts of our globe.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 October 24 - Mir News 331: Progress-M33. 

    The launch of this freighter is on schedule for the midst of November. The exact date has not yet been set. The delay has been caused by problems in the delivery of the Soyuz-U carrier.

    First EVA:

    If Progress-M33 will be launched as planned and the docking at the Mir station will be successful, the crew of the 22d Main Expedition to Mir will make the first spacewalk (EVA) on 21.11.1996. During this EVA the cosmonauts will have to deploy and connect cables for a new solar panel.

    Radio-amateur traffic: The repeater of the radio amateur installation in the Priroda module is fully operational and traffic can be monitored almost every pass on frequency 437.950 mc (+ and - for Doppler shift). The crew uses 145.550 mc for own phone contacts. The Russians use the call R0Mir; John Blaha uses his official call KC5TZQ. Valeriy Korzun expects to get his own Russian call in the future. 145.550 mc is still in use for packet radio traffic.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 October 29 - Mir News 332: Progress-M33. 

    The last estimated date for the launch of this freighter is 17.11.1996.

    Radio-amateur traffic:

    As of 1.11.1996 the Mir crew (call sign R0Mir) will use new frequencies for VHF-traffic. Packet radio: 145.800 mc; Voice, downlink: 145.200 mc, uplink 145.800 mc. These frequencies had been recommended by the International Amateur Conference for Region 1.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 November 13 - Mir News 333: Progress-M33. 

    The delayed launch of this freighter is now on schedule for 19.11.1996 at 2320 UTC (for Moscow then already 20.11.1996). Progress-M33 will bring food, water, fuel, post, spare parts, etc. to the station. The crew is anxiously waiting for containers for the collection of 'human waste' . The available containers are as good as full and the crew has to 'improvise' measures to keep this situation under control. They did not complain about this problem, but have no appreciation for the fact that TV-stations in Russia made it public as this caused anxiety among their relatives. There also has been a publication about the fact that their vacuum cleaner was out of order. Korzun denied this. Jokingly he supposed that someone produced this disinformation to get more money from the taxpayers for spaceflight.

    Communications: Mir is passes take place during the day hours and a lot of radio traffic can be monitored. During the 5th pass within our range Mir is no longer in range of Russian tracking stations. Now and then the tracking station of ESA, Oberpfaffenhofen, relays Mir-TsUP communications during that pass. The packet radio installation is regularly in use for radio-amateur traffic on 145.800 mc. This P/R installation now and then is used for service traffic on 143.625 mc. This is not always successful and then TsUP used the old RTTY installation as an alternative.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 November 19 - Progress M-33.  Spacecraft: Progress M. Mass: 7,190 kg (15,850 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 22 Nov 1996 01:01:30 GMT. Undocked on 6 Feb 1997 12:13:53 GMT. Thereafter in independent orbital flight in a 377 x 395 km x 51.65 deg orbit. Failed to redock with Mir on 4 Mar 1996. Destroyed in reentry on 12 Mar 1997 03:23:37 GMT. Total free-flight time 35.70 days. Total docked time 76.47 days.

  • 1996 November 20 - Mir News 334: Successful launch freighter Progress-M33. 

    This long-expected freighter blasted off from Baykonur on 19.11.1996 at 23 hrs 20 mins and 35 seconds UTC (for Moscow-time and for MEWT already on 20.11.1996). After some orbits the beacon- and TLM-transmissions could be monitored over here. The cargo of Progress-M33 consisting of post, food, spare-parts, containers for human waste and materials for experiments weighs 1650 KG. In the tank-compartment of Progress-M33 547 KG oxygen, fuel and water has been stored. Fuel for the Mir-complex itself weighs 2462 KG. Also among the 547 KG a new supply of nitrogen for the pressurising and purging of the oxygen-producing Elektron systems. Because of the fact that there will be no further deliveries of supplies before New Year the mail-bag also contains the Christmas- and New Year post for the crew.

    Progress-M32: This old freighter has to free the port at which she is docked now for the arrival of the Progress-M33. This is the aft docking port (Kvant-1, +X-axis). Progress-M32 can abandon the Mir-station for the systems of her successor are working normally. This will take place on 20.11.1996 at 1945 UTC. After a few orbits Progress-M32's engines will be fired for the de-orbit manoeuvre after which Progress-M32 will burn up over a designated area in the Pacific East of New Zealand.

    Expected time of arrival and docking Progress-M33 at Mir:

    This will be on 22.11.1996 at 0100 UTC. Progress-M33 has to approach and dock in the automatic mode by the system Kurs. If this system fails commander Korzun is ready to conduct the freighter manually with the system TORU.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 November 22 - Mir News 335: Progress-M33 successfully docked at Mir. 

    The Progress-M33 linked up with Mir on 22.11.1996 at 010130 UTC. Approach and docking were executed in the automatic mode with the system Kurs. Until the soft mate Korzun was prepared to take over manually with TORU if necessary. During the first pass of Mir in orbit 61467 from 0050-0056 UTC Korzun reported about the approaching freighter. At 0556 UTC TsUP gave permission for the docking. Already during the pass in orb. 61468 from 0223-0234 UTC the crew reported that they had opened the hatch and that they enjoyed the fresh air which flowed in and the smell of apples.

    Progress-M32: This old freighter separated from Mir on 20.11.1996 at 194414 UTC. The same day at 224218 UTC the de-orbit burn took place and she burnt up over the Pacific East from New Zealand.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 November 27 - Mir News 336: 1st Spacewalk (EVA) crew 22d Main Expedition to MI. 

    The crew of the 22d M.E. to Mir, Korzun and Kaleri, will do this EVA on 2.12.1996 between 1550 UTC (opening hatch) and 2130 UTC (closure hatch). During this EVA they will have to install extra cables and contacts for a solar panel on the outer surface of the astrophysical module Kvant-1 (Module-E). This solar panel had been installed over there in May 1996 by Onufriyenko and Usachov. This panel had been delivered to Mir by Atlantis on 15.11.1995 during mission STS-74 as cargo on the docking compartment. At the outer surface of that compartment 2 solar batteries had been stowed, 1 Russian and 1 American. In May 1996 the American one had been installed and partly connected. That is why the solar panel could deliver not more than 3 kW. If the work during the 1st EVA will be accomplished successfully the panel can deliver 6 kW electrical power. During the EVA John Blaha will remain inside the complex to assist and take care for the communications.

    Radio communications during this EVA:

    During passes on 143 mc, but somewhat lower than 143.625 mc and possibly via the 2 available geostationary Altair-satellites.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1996 December 2 - EVA Mir EO-22-1.  Spacecraft: Mir.

    Began installation of MCSA solar array cables.

  • 1996 December 3 - Mir News 337: 1st Spacewalk (EVA) crew 22d Main Expedition. 

    Korzun and Kaleri did this EVA on 2.12.1996 between 1554 and 2151 UTC (duration 5 hrs. 57 mins). They had to deploy and connect cables to the American solar panel on the outer surface of Kvant-1. They accomplished their task successfully and without problems. The solar panel has been checked and can deliver a current of 80 Amperes. When Mir for the first time came within our range (orbit 61636, 2015-2022 UTC) the cosmonauts were still working near the Sofora girder. Somewhat later they returned to the airlock. During the 2d pass for our position (orb. 61637, 2149-2159 UTC) Korzun reported the closure of the hatch at 2157 UTC. Regularly John Blaha could be heard in contacts with TsUP and the cosmonauts. Inside the Mir- complex he assisted the cosmonauts, checked systems and executed commands given to him by TsUP. While Korzun and Kaleri were still in the airlock to equalise the air pressure Blaha in co-ordination with TsUP loaded control-data in the central computer. On 3.12.1996 at abt. 0108 UTC, everybody, your scribe inclusive, though tired but satisfied, went to sleep. 2d EVA 22d M.E.: This EVA is on schedule for 9.12.1996. During this EVA Korzun and Kaleri will have to accomplish the following tasks: 1st: The mounting of Rapana on the 3d truss construction at the outer surface of the Kvant-1 module: 2d: The installation of a new Kurs-antenna on the transition section (P.Kh.O.). Chris v.d. Berg, NL-9165/A-UK3202

  • 1996 December 9 - EVA Mir EO-22-2.  Spacecraft: Mir.

    Completed external cable installation for MCSA solar array. Installed antenna.

  • 1996 December 10 - Mir News 338: 2d Spacewalk (EVA) 22d Main expedition. 

    This EVA took place on 9.12.1996 between 1352 UTC (opening hatch) and 2028 UTC (closing hatch). So a duration of 6 hrs 36 mins. The EVA lasted longer for Korzun wished to accomplish all what had to be done and there also was a problem with something which bungled loose. Before return they restored the connection of the radio-amateur antenna for the 145 mc. Probably this antenna had been disconnected by accident during the 1st EVA. They connected the antenna again and while they were flying over Chile and Brazil they asked John Blaha to listen out on the 145.800 mc to check whether the antenna was working or not. There was no traffic on that frequency in that area and so they had to wait until they came in range of European amateurs. I asked the English radio-amateur Pat Gowen (G3IOR) to give calls on 145.800 mc as soon as Mir would come in range (at abt. 1934 UTC). So he did and these signals could be heard by John Blaha while Mir was flying over France. He reported this to the still being on EVA Korzun and Kaleri and congratulated them with their success. Korzun urged John not to transmit, but to listen only. The cosmonauts fully accomplished their tasks: installing the truss construction Rapana at the truss Ferma-3 and the replacement of the Kurs-antenna on the outer surface of the P.Kh.O. (transition section). John Blaha who stayed inside the complex took care of the communications and executed commands given to him by TsUP. He gave the cosmonauts all possible moral and technical help. The cosmonauts and Blaha did an excellent job during this EVA, they gave an example of fruitful international co-operation and so they all deserve a loud: 'MOLODTSY' (very well done). Of course the cosmonauts were very tired after the EVA and back in the airlock they had to do hard labour to put off their spacesuits. Just before midnight Korzun could be heard in a contact with a Portuguese radio-amateur via the repaired antenna for the 145 mc.

    Thus far there are no more EVA's on schedule for this crew.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 January 3 - Mir News 339: Solar-orbit. 

    As of 1.01.1997 the Mir-complex will remain in a so called solar-orbit for 1 week. This means that the Mir remains in the sunlight and has no shadow periods. While large areas on the Northern Hemisphere experience very low temperatures these are high on board the space-station. The cosmonauts and the astronaut have to wear airy clothing. Periods like this are very good for the execution of space-walks (EVA-s), but regretfully there are no more EVA-s planned for this expedition.

    Communications: Now and then the (almost) geostationary satellite Cosmos-2054 (Altair-1) is used for the TsUP-Mir communications. This satellite is standing over 16 dgs West. Sometimes the satellite is used for phone only, but more often to exchange TV-transmissions. On 27.12.1996 during orbit 62024 Korzun explained the experiment Volna and the behaviour of liquids in this instrument could be seen. They use the Altair-1 satellite also for interviews, press-conferences and Packet radio for reception and transmission of radiograms. In the near future the DLR-ground facility in Oberpfaffenhofen will use this satellite for direct contacts with European astronauts.

    Radio-amateurism: On 1.01.1997 the crew changed the frequencies for radio-amateur traffic in the 145 Mc band. They now also use duplex (split) for Packet radio traffic. They changed the frequencies as follows: Uplink (transmissions to Mir) for Phone and P/R 145.200 Mc; downlink (from Mir to Earth, for Phone as well as for P/R 145.800 Mc. Changes like this can always be expected: the change which is suitable for 1 region might be unfavourable for other regions. This change is very good for the amateur-satellite band between 145.800-146 Mc as strong ground stations no longer hamper weak Oscar downlink signals around 145.800 Mc.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1997 January 12 - STS-81.  Spacecraft: Atlantis. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    After a night launch of Space Shuttle Atlantis, the Shuttle docked with Mir at 03:55 GMT on January 14. STS-81 transferred 2,715 kg of equipment to and from the Mir, the largest transfer of items to that date. During the docked phase, 640 kg of water, 515 kg of U.S. science equipment, 1,000 kg of Russian logistics, and 120 kg of miscellaneous material were transferred to Mir. Returned to Earth aboard Atlantis were 570 kg of U.S. science material, 405 kg of Russian logistics and 98 kg of miscellaneous material. At 02:16 GMT January 19, Atlantis separated from Mir after picking up John Blaha, who had arrived aboard STS-79 on September 19, 1996, and dropping off Jerry Linenger, who was to stay aboard Mir for over four months. The Shuttle backed off along the -RBAR (i.e. toward the Earth) to a distance of 140 m before beginning a flyaround at 02:31 GMT. Most of the flyaround was at a distance from Mir of 170 m. The first 'orbit' around Mir was complete at 03:15, and the second was completed at 04:02 GMT. Then the Orbiter fired its jets to drift away from the orbit of Mir. NASA's first Shuttle mission of 1997 came to a close with a landing at the Kennedy Space Center at 14:22 GMT on January 22 (after the first opportunity was waved off due to cloud cover at the Cape).

  • 1997 January 14 - Mir News 340: Atlantis/Mir. 

    Atlantis (mission STS-81) has been launched on 12.01.1997 at 09.27.33 UTC for her 5th docking mission. At 0950 UTC Atlantis was within our range and commander Baker could be heard on 259.700 Mc AM/W in a short contact with Houston via Zaragossa in Spain. The rendezvous operations will begin on 14.01.1997 at 2212 UTC. Atlantis arrives near Mir on 15.01 at 0247 UTC and will dock 15.01 at 0353 UTC. Let us hope that the docking will take place a few minutes earlier for the window during the first pass of both enormous objects within our range will close at 0352 UTC. Hard mate will take place on 15.01 at 0427 UTC and the hatches will be opened on 15.01 at 0537 UTC. John Blaha will conclude his experimental activities on board Mir with some experiments related to the docking and immediately thereafter he will be relieved by Jerry Linenger. Blaha will remain in space for a while as payload specialist on board Atlantis and Linenger will continue his flight as 2d Board Engineer/researcher in Mir.

    Radio traffic: If they stick to the same frequencies as in the past we can expect radio traffic on 121.750, 130.165 and 143.625 Mc. Extensive use of the American TDRS-s after the docking van be expected. Possibly the Russians will now and then use their (almost) geostationary satellites Altair-1 and 2. During the 4th docking mission (STS-79 in Sept. 1996, most communications took place via the American TDRS-s.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 January 15 - Mir News 341: Atlantis links up with Mir. 

    The soft docking took place on 15.01.1997 at 03.54.57 UTC so almost 2 minutes later than planned. Radio communications revealed that Houston preferred to perform the docking when both objects were in daylight. In comparison with the last docking mission (STS-79) there was more radio traffic on the Mir-frequencies. This had been caused by some problems the Shuttle had with communications with Houston. During the first pass of both objects in Mir's orbit nr. 62313 the approach was in its final phase. At 035106 UTC Korzun reported that the 'final approach' was going on, that permission for the docking had been given and that the distance between Mir and Atlantis was abt 6.5 Meters. During the next pass over here in orb. 62314 again a lot of radio traffic conducted by Korzun and Blaha. Blaha told his 'successor' Linenger that Houston had asked to inform Atlantis that they had to connect an antenna for communications with Houston. The Mir crew was in the SO (docking compartment at the Kristall module) and had already opened the hatch from that side. This had taken place at 052918 UTC. The opening of the hatch between Shuttle and Mir was far behind schedule due the above mentioned communication problems. In the SO the Mir-trio was cutting capers and making gestures to urge Baker to open the hatch. The permission to open that hatch should have been given at 054321 UTC. Possibly they wished to blow a lot of fresh air in the fusty Mir-atmosphere before opening. At last the hatch swung open at 055754 UTC and Baker and Korzun met each other and he and the rest of the Shuttle crew invaded Mir. After the welcome ceremony the first activity was the transfer of the seat liner for Linengers place in the Soyuz-TM24. When this work had been accomplished Linenger was a crew member of Mir. Officially this was at 0945 UTC. In orbit 62315 Mir communicated with TsUP Moscow via Altair-1. In the beginning they transmitted recordings of the approaching Atlantis and later on images of both crews in Mir. After the transmission of images they continued this contact with speech. In this period the huge Atlantis/Mir combination could be seen passing almost through the zenith as a very clear star. This was at 070012 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 January 20 - Mir News 342: Atlantis/Mir. 

    During the period in which Atlantis and Mir were linked together the American TDRS-facilities were in use for the bulk of radio communications, thus anticipating the communication procedures of the future International Space Station Alpha. The Russians used their facilities only to discuss matters regarding the Mir-complex itself. With a few exceptions the Atlantis also took care for the movements (attitude) control of the huge space combination.

    Atlantis separated from the Mir:

    Atlantis undocked from the Mir on 20.01.1997 at 02.15.44 UTC. At 0357 UTC the engines of the Atlantis gave the separation burn for the ride home. After the undocking Atlantis remained in the free drift until the distance permitted firing of steering rockets. During the 2 flights of Atlantis around the Mir-complex no images have been transmitted from Mir. These had been recorded and transmitted to Earth later that day via Altair-1. Among them good images, for instance Atlantis flying away from under a Mir solar panel and several views of Atlantis moving away with a sight of the Earth in the background.

    Soyuz-TM25: The next important operation will be the launch of Soyuz-TM25 from Baykonur on 10.02.1997 at 1409 UTC. Soyuz-TM25 will bring the 23d Main Expedition (Tsibliyev and Lazutkin) and the German astronaut Ewald to the Mir. (Stand-in crew: Musabayev, Budarin and Schlegel)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 January 22 - Landing of STS-81. 

    STS-81 landed at 14:22 GMT with the crew of Baker Mike, Jett, Wisoff, Grunsfeld, Ivins and Blaha aboard.

  • 1997 January 28 - Mir News 343: Soyuz-TM25. 

    This ship with the crew for the 23d Main Expedition (M.E.) to Mir, Tsibliyev and Lazutkin, and German's Mir'97 astronaut Reinhold Ewald is on schedule for launch from Baykonur on 10.02.1997 at 1408 UTC. The call signs of this crew are Sirius-1, 2 and 3. If all goes according to plan Soyuz-TM25 will dock at Mir on 12.02.1997 at abt 1553 UTC. Ewald will stay on board for 18 days and return to Earth with the relieved crew of the 22d M.E., Korzun and Kaleri. During the Mir'97 mission DLR's GSOC in Oberpfaffenhofen will be able to communicate directly with Mir via VHF-channels, but possibly also via the quasi-stationary Cosmos-2054 (Altair-1) over 16 degrees W.L. On 4 and 5.12.1996 GSOC in Oberpfaffenhofen tested communications via Altair-1 and meanwhile the intention to use this possibility during Mir'97 and future Euromir missions has been officially confirmed.

    Mir-routine: The American astronaut Linenger started with his experimental programs. He is very pleased to be on board Mir and had less problems as his countrymen during previous flights in finding things for his work. Of course he did not found all he needs, but obviously the experience of his predecessors led to improvements in that field. He emphasised

    Hij legt by zijn experimenten erg de nadruk op lichamelijke oefeningen, waarbij hij zich behoorlijk inspant. De samenwerking met zijn Russische collega's is uitstekend. Linenger is ook goed ingewerkt door zijn voorganger Blaha. Voor wat betreft zijn werkplanning en de manier, waarop de resultaten van zijn experimenten de geleerden op aarde moeten bereiken, heeft hij aan de Amerikaanse consultatieve groep op het TsUP by Moskou een aantal voorstellen gedaan.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 February 10 - Soyuz TM-25.  Spacecraft: Soyuz TM. Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-23. Soyuz TM-25 docked with Mir at the forward port on February 12 at 15:51:13 GMT.

  • 1997 February 10 - Mir News 344: Launch Soyuz-TM25. 

    This ship with on board the relief crew for the 23d Main Expedition (M.E.) to Mir and the German astronaut Reinhold Ewald, who will in co-operation with the Russians execute the Mir-97 program, has been launched from Baykonur on 10.02.1997 at 14hrs 09mins 30secs UTC. The call sign of the crew is Sirius (so Sirius-1, 2 and 3). The commander is Tsibliyev, now making his 2d flight in space and the board-engineer is Lazutkin who did not fly thus far.

    Progress-M33: There must always be a free docking port for the new ship. Before the flight of the Soyuz-TM24 the Russians undocked the Progress-M as soon as they were sure that the systems of the new ship were functioning normally, so at abt 1 day after launch. Some orbits after the undocking the freighter entered the earth's atmosphere and burnt up. To begin with the Progress-M32 the Russians changed this routine and the Progress-M32 flew autonomously until 18.08.96, redocked to the complex and left Mir and burnt up in the atmosphere on 20.11.1996. The Progress-M33 separated from Mir's aft (Kvant-1 +X axis) on 6.02.1997 at 12hrs 13mins 56secs and will make an autonomous flight until the beginning of March '97.

    Soyuz-TM24: This ship had been docked at the forward docking port (transition section - P.Kh.O. -X axis). This port has been chosen for the docking of the Soyuz-TM25. In the future the Russians refrain from the use of the approach system Kurs in Soyuz-TM and Progress-M ships. This decision has been taken due to problems about the delivery of that system between RKK Energiya and the factory NPO Kharton in Kharkov, Ukraine. On 7.02.1997 at 16hrs 28mins 01secs the Soyuz-TM24 separated from Mir and manned by Korzun, Kaleri and Linenger made an autonomous flight concluded by the docking of that ship at the aft (Kvant-1 +X axis) docking port that day at 16hrs 51mins 27secs. Undoubtedly this has been quite an experience for Jerry Linenger who came by Atlantis and will return with the shuttle.

    Dockings of Soyuz-TM ships will be executed manually by the commander and those of unmanned Progress-M freighters will be done by the crew on board Mir by the use of the Remote Control system TORU.

    ETA (expected time of arrival) of Soyuz-TM25 at Mir:

    Soyuz-TM25 has to dock to the Mir's forward (P.Kh.O. -X axis) docking port on 12.02.1997 at abt. 1550 UTC. This is 3 minutes after the first pass for both objects over Western Europe. During this pass (1541-1547 UTC) we can expect communications about the approach on 121.750 mc FM-N and the 143.625 mc.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 February 12 - Mir News 345: Soyuz-TM25 docked at Mir-complex. 

    Without significant problems Soyuz-TM25 docked at the aft (+X axis) of Mir on 12.02.97 at 15.51.13 UTC. During this operation the Russians still used the system Kurs. The automatic mode worked well from the beginning and only in a distance of 5 M. Tsibliyev had to take over manually due to a slight deviation along the X axis (roll). After some little corrections he accomplished a soft 'kasaniye' (touch). During the first pass of both objects for our position (orb. 62758) 1541-1548 UTC approach traffic could be monitored on 121.750 mc, but the full Altair-1/Mir window (1510-1618 UTC) was in use for this traffic. In fact Soyuz-TM25 used for communications with TsUP 2 relay facilities: Mir and Altair-1. In this traffic Tsibliyev and Lazutkin (Siriusy) as well as Korzon (Fregat) could be heard. The moment of the soft docking could be derived from the word 'congratulations' spoken by one of the cosmonauts. During the next pass (orb. 62759), 1720-1726 UTC, the hatch had already been opened and the pass thereafter (orb. 62760/61) the new crew was inside Mir.

    Communications Soyuz-TM25: 3 hours after launch on 10.2.97 (orb. 2, 1712-1714 UTC) the transmissions of the ship could be monitored on the well known frequencies with Tsibliyev on 121.750 mc with TsUP. During the next pass (1841-1848 UTC) he reported the good results of the 2 orbit corrections. He also mentioned some problems with a TV-installation or a screen. Apart from some interference by the ground services of a near by airport (also using 121.750 mc, but AM-W) the signals came in loud and clear. Also during the second day (11.02.1997) traffic could be heard during all passes for our position.

    Communications Mir: On 8.02.1997 DLR's GSOC in Oberpfaffenhofen (Germany) and Mir tested the direct link via the quasi-geostationary comsat Altair-1 over 16dgs West. Good images and audio from inside Mir demonstrated that the test was a great success. They also checked the performance of the so called BDD (Betriebstechnik Deutschland Direkt). This is an interface assembly for direct data exchange between specialists on earth and Reinhold Ewald during experiments in the framework of the Mir-97 program. A few days later it was clear that the direct link between GSOC and Mir will be a normal routine until 2.03.1997 (the end of Mir-97).

    PS: A tragic event in my family caused delay in the mailing of this report.

    Chris v.d. Berg, NL-9165/A-UK3202 E-mail: cmvdberg@worldaccess.nl

  • 1997 February 22 - Mir News 346: Mir'97. 

    Dr. Reinhold Ewald amuses himself well on board of the Mir space station. He uses as his private domain the Module Kristall (T). His American colleague Linenger has his private quarter in the Module Spektr (O). He is sleeping there , has room for personal belongings and he found a free surface on the wall to fasten some photographs. Thus far I do not know the temporary private quarters of Tsibliyev and Lazutkin. Korzun will remain in command of the complex until his departure on 2.03.1997. Ewald discusses the experiments which he has to execute during this mission with Sigmund Jähn (at TsUP) or with Hans Schlegel (in GSOC). From the radio traffic could be derived that Ewald is successfully executing the program although now and then something goes wrong. This was the case with an experiment planned for 19.02.1997: In the framework of a medical experiment he had to drink 200 ml tomato-juice with salt, but bad quality of the juice made this impossible. The experiments with the Titus-oven, the French Alice-2 installation (studies of the characteristics of liquids) and MEDEX (medical experiments) have been successfully executed thus far.

    Anniversaries: On 20.02.1997 Tsibliyev celebrated his 43d birthday. Exactly 11 years ago the Base block of Mir was launched. . Problems with a gyrodyne: On the eve of these anniversaries the crew had to solve a difficult problem. On 19.02.1997 during the pass in orbit 62876 (1521-1527 UTC) TsUP gave Korzun data, which had to be loaded in the system Svet for the movements control of the complex. Korzun asked what the reason was. TsUP informed him that Telemetry showed the malfunction of a gyrodyne in Kvant-2 (Module-D). In the evening and night the crews solved the problem.

    Communications: Contrary to the expectations the German GSOC Oberpfaffenhofen seldom uses the possibility for direct links with Mir via the (almost) geostationary Altair-1 (Cosmos-2054). Apart from the 143.625 mc, Ewald regularly uses the so called UKW-2 (VHF-2) on 130.165 mc for communications with his consultants (Sigmund Jähn) at TsUP and (Hans Schlegel) in GSOC. Now and then Linenger can be heard on that frequency with the American consultative group at TsUP . The 145.800 mc is the downlink frequency for Packet radio or phone. Mostly Korzun can be heard here. A few times Ewald uses this facility for contacts with German radio-amateurs. He uses the call sign DL2Mir. In the simplex mode he sometimes can be heard on 145.925 mc.

    Chris v.d. Berg, NL-9165/A-UK3202 E-m: cmvdberg@worldaccess.nl

  • 1997 February 24 - Mir News 347: FIRE ON BOARD OF THE Mir-SPACE STATION. 

    Radio traffic during VHF windows for our position in the morning of 24.02.1997 revealed that something serious had happened on board Mir. Somewhat earlier there was already an indication: a direct TV-link from Mir with Oberpfaffenhofen via Altair-1 for this morning did not take place. During the 3d pass for our position (orb. 62943, 1341-1348 UTC) the cloven hoof came out: in a conversation with his consultants on earth Ewald reported about a fire on board. This fire broke out last night. An oxygen cartridge caught fire and a grey smoke spread out in all parts of the complex. Korzun and Kaleri fought against the fire with extinguishers and the others tried to push back the smoke. All crew members had to wear gas-masks. This lasted two and a half hours the maximum endurance of those masks. The extinction water caused a high humidity and the temperature of the atmosphere was higher than normal. Ewald did not get smoke or just a little bit in his longs and to remain on the safe side he swallowed coal- and vitamin tablets and milk products. He was very tired but he did not think that this had been caused by something like pollution, but by the lack of sleep. He went asleep at 6 o'clock in the morning and woke up 4 hours later. Jerry Linenger was very busy collecting air samples for pollution tests. He also tried to determine the amount of formaldehyde. The crew of six was in the Base Block when the fire began in an adjacent room. Russian toxicologists are analysing telemetric data about Mir's on board atmosphere. The crew already collected urine- and saliva samples and later on they got instructions to collect blood samples and to do additional medical tests. In the course of the day a TV press conference was on schedule and a lot of journalist were waiting in Oberpfaffenhofen. Ewald told that the events had caused such a mess in the station that it was not convenient to have that TV session today. As a palliative Ewald answered some questions about the nightly occurrences and his statements almost fully confirmed the information gathered by me for this report.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 March 2 - Mir News 348: Soyuz-TM24 made happy landing. 

    On 2.03.1997 at 0644 UTC the return capsule of the Soyuz-TM24 made a safe landing in Kazakhstan not far from Arkalyk (47degr49min North; 69degr24min East). At abt 4 mins later the first helicopter of the search- and rescue team reached that position. The return operation and landing took place without problems. During the return operation Soyuz-TM24 communicated via the Eastern tracking stations in Russia and probably Altair-2 over 96 dgs East. Obviously Altair-1 was (or: is?) not operational.

    Last week of Mir'97 and Main Expedition Mir 22:

    The fire in the night from 22 to 23.02 put its stamp on this last week due to the pollution of the Mir's atmosphere during the first days and the extra attention the crew had to give to the damaged oxygen-generator and cables. For a long time there was the smell caused by the fire. One of the cosmonauts spoke about the smell of 'roasted turkey'. Some crew members suffered from some irritation of the bronchia, a dry throat and sleeping problems. Nobody was hurt with the exception of Korzun who had a very small burn on his hand. Ewald had already executed the majority of the Mir'97 experiments and the events did not significantly influence that program. German project managers were satisfied about the successful results and conclusion of the mission. During this week there has been a lot of radio traffic on 2 frequencies simultaneously: the Russians used 143.625 mc and Ewald and Linenger 130.165 mc. For some planned TV sessions, i.e. for the RTL children's programme Captain Bluebear and about a contest for drawings by children with the wife of the German President Herzog they did not use the geostationary satellites but direct TV transceivers on lower frequencies. For phone during these sessions Ewald used the UKW-2 130.165 mc.

    Siriusses: The new crew, Tsibliyev and Lazutkin, the 23d M.E. to Mir, and Jerry Linenger will have to do a lot of work in the near future. In fact there are still a lot of experiments in the framework of Mir'97 to be done: this had been planned and this work got the designation Mir'97E, the letter 'E' standing for 'Extension'.

    Progress-M33: This old freighter is still flying autonomously until her 2d docking at Mir. That will take place on 4.03.97. Tsibliyev got orders to control the approach and docking manually with the remote-control system TORU. There has also been an instruction to leave Progress-M33's hatch closed after docking. Kaleri asked TsUP to consider the possibility to open the hatch and to use the still available room in the spherical part of Progress-M33 to stow stuff no longer needed: especially the considerable amount of human waste. During the long period with a crew of 6 the quantity of this increased enormously.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 March 2 - Landing of Soyuz TM-24. 

    Korzun, Kaleri and Ewald undocked from Mir in the Soyuz TM-24 spaceship at 03:24 GMT on March 2 and landed at 06:44 GMT near Arkaylk in Kazakstan.

  • 1997 March 4 - Mir News 349: Set-backs. 

    Two serious disadvantages vex Russian spaceflight:

    1. Progress-M33:

    The redocking of this freighter at the Mir complex planned for 4.03.1997 at 0750 UTC did not take place. During the first pass of both objects here in Mir's orb. 63065, 0733-0739UT, radio traffic revealed that the docking was not possible. Tsibliyev reported that the Progress-M33 did not do what she had to do and that he did not have a continuous image on his screen of the approaching ship. So he was unable to aim her with the system TORU. He was able to give some commands, for instance to reduce the speed of Progress-M33. Progress-M33 passed Mir in a distance of appr. 220 - 230 Meters. The cosmonauts now and then had visual observations of the Progress-M33, but not continuously and it was difficult to determine the distances via the portholes as there were no reference points. Radio traffic during following passes confirmed the failure. Progress-M33 was flying near Mir in a distance of appr. 1 KM. A commission headed by V. Solovyov is trying to find the cause of the failure and to find a solution. Tomorrow they hope to announce if and, if so, when the second attempt will take place.

    2. Geostationary communications for the Mir-space station:

    At the moment Mir does not have the possibilities to communicate via Altair-1 (Cosmos-2054) and Altair-2 (Luch-1). Altair- 1 came in a so called sun-pointing attitude and is no longer under control. This happened once in the past and then the satellite restored the normal attitude itself. Whether this will be possible this time or not is not sure. Mir also cannot use the 2d geostationary satellite over 96 degrees East. The Antares transceiver for Mir's uplink to the geostationary satellites is unserviceable and has to be replaced. The Russians hope to send a new Antares to Mir by Progress-M34. So the communication situation is very poor at the moment: in fact even worse than before the deployment of Luches for Mir. In the past tracking ships filled up the gaps, but these ships are not operational now. The possibility to use American tracking stations (Wallops, White Sands and Dryden) does not give enough solace.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1997 March 7 - Mir News 350: SITUATION ON BOARD Mir REMAINS PRECARIOUS. 

    After the loss of one Solid Fuel Oxygen Generator in the night from 23 to 24.02 the crew has been struggling along to keep the mini-atmosphere on board of the space station suitable for the needs of human beings. On 5.03 one of the Elektrons (possibly the 2d Elektron is out of order and has to be repaired with spare parts to be delivered by the next supply ship) showed a malfunction and so the crew had to use a part of the oxygen reserved for spacewalks to bridge the period until the repair of that Electron. They managed to get this Elektron operational again in the afternoon. The crew is very busy to secure the working of the life systems and this fact can be derived from radio traffic during every possible pass. Among the additional measures to maintain a liveable situation on board a lot of air hoses have been deployed to enhance the air circulation through the whole complex.

    Communications: As it is not possible to communicate via the geostationary satellites every possible VHF-pass via tracking stations in Russia and the United States is fully utilised. In this way I can obtain a lot of information, but in fact this is rather poor in comparison to that what can be derived during the long sessions via Altair-1. For TV-sessions the Russians now use the direct links on lower frequencies via tracking stations. These sessions are shorter and have a rather poor quality, mostly black/white and often the accompanying speech goes via the normal VHF-downlink.

    Progress-M33: It has been decided not to try a second attempt to redock Progress-M33 at Mir. The Progress-M33 will be put on a destruction course on 11 or 12.03.1997 and burn up in the atmosphere over a designated area in the Pacific East of New-Zealand.

    Progress-M34: The Russians are still waiting for the disposal of a rocket for this launch. This certainly will not be earlier than 25.03.1997. They hope to launch the Progress-M34 on 6.04.1997. Among a lot of other supplies this Progress has to deliver a replacement for the Antares transceiver (uplink to Luches) and spare parts and materials for the repairs of the defective life support systems.

    Spacewalk (EVA): The Russians still hope that Tsibliyev and Linenger will be able to do an EVA. For the time being 17.04.1997 is on schedule.

    Chris v.d. Berg, NL-9165/A-UK3202

  • 1997 March 21 - Mir News 351: Mir-routine. 

    Gradually the passes of Mir for our area shifted to the night hours, but nevertheless a lot of radio traffic could be monitored since the last Mir-report. This traffic revealed that the only system for the production of oxygen is the solid fuel oxygen generator. The crew co-ordinates the use of the so called 'shashki' (disks) with TsUP and daily abt 3 of those 'cartridges' are 'burnt'. In the beginning they still tried to activate the only operational Elektron to generate oxygen from 'technical' water, but possibly the gas-analysers reported that the quality of the production did not reach the desired standards and they had to stop these attempts. They seem to have enough 'shashki' until the arrival of new supplies but they cannot use all available cartridges. They got orders to refrain from the use of those produced in the years after the decay of the Soviet Union.

    Progress-M34: The launch of this badly needed freighter is on schedule for 6.04.1997. It is not sure whether or not spare parts (filters a.s.o.) are ready before that launch. The Progress-M34 will also have to deliver a new Antares transmitter for communications via the now only available Altair (nr. 2) satellite.

    Communications: The present position of Altair-2 is over 94 degrees East. For docking operations of Soyuz-TM ships and shuttles, but also for the communications during EVA-s and the morale of the crew a position more to West, for instance in the slot of Altair-1 (Cosmos-2054) would be more suitable.

    Movements control: On 19.03.1997 during the pass in orbit 63298, Tsibliyev reported a malfunction of an Omega angular rate sensor. At 0448 UTC the SUD (movements control system) showed a failure and the complex came in an inexplicable rotation. Apart from one the gyrodynes were still working, but obviously unable to correct the stations attitude. During the next pass (in orb. 63300, 0856-0906 UTC) the crew got orders to shut down the gyrodynes. The station came in a so called free drift and from there the attitude had to be corrected by steering jets. These events caused a decrease of electrical power due to bad orientation of the solar batteries towards the sun. So for some hours the crew had to restrain power consumption. Next day's radio traffic revealed that the situation was almost under control. The crew worked hard to make another Omega sensor operational and doing so they met a lot of problems with the deployment of cables.

    Jerry Linnenger: In contradiction to the beginning of his mission contacts of Jerry with the American consultative group at TsUP Moscow could not be monitored for some weeks.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 3 - Mir News 352: Progress-M34. 

    The launch of this freighter from Baykonur is on schedule for 6.04.1997 at 1904 UTC. If this start will take place and the flight to the Mir complex will be successful docking can be expected on 8.04.1997 at abt. 1730 UTC. Progress-M34 has to deliver new supplies of fuel, oxygen, water, food and repair materials. Progress-M34 will also bring 2 spacesuits for spacewalks (EVA's) of a new type. Originally the Russians planned to have a new Antares transmitter (for communications via the geostationary satellite) ready for the flight with Progress-M34, but possibly they cannot make that and that means that this transmitter will be delivered at Mir by the shuttle Atlantis in May.

    Mir-routine: Mir's passes for our position take place during the night hours and in this period all communications are handled by the tracking stations in the USA Dryden and Wallops and the OKIK's in the East of Siberia. For the oxygen production the crew is fully dependent on the so called 'shashki', the lithium perchlorate cartridges. Daily they 'consume' 2 or 3 cartridges. The 2 Elektron systems could not be repaired and so the crew has to wait for new Elektrons to be delivered by Atlantis.

    Altair-2 (23426 - 94082A): This geostationary satellite recently still over a sub-satellite point over 95 degrees East has been brought in a somewhat higher orbit. Now the period is more than 1436 minutes. This means that the sub-satellite point is slowly moving to the West. if all goes according to plan Altair-2 will reach a position over 16 degrees West in the 26 week of May.

    1st Spacewalk (EVA) Tsibliyev and Linenger: This EVA is on schedule for 29.04.1997.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 6 - Progress M-34.  Spacecraft: Progress M. Mass: 7,156 kg (15,776 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. It carried supplies for the Mir station and repair equipment for Mir's oxygen generators, replacement oxygen-generating 'candles' and a pair of new spacesuits. Docked with Mir at the rear Kvant module port on 8 Apr 1997 17:30:03 GMT. The Mir complex raised its orbit by 5 km on 15 Apr 1997 at 12:00 GMT, using Progress M-34's engine. Undocked on 24 Jun 1997 10:22:50 GMT. It was then used to perform a redocking test using newly developed remote-control procedures which were to replace the automatic system that Russia could no longer afford to buy from Ukraine. At 25 Jun 1997 09:18 GMT Mir commander Tsibliev was remotely commanding the approach of Progress to the Kvant module. This involved guiding the Progress via a television monitor. The Progress was difficult to see against the cloudy earth background at the time of the attempted docking. It went off course and collided with a solar array on the Spektr module and then the module itself. A large hole was made in a solar panel, one of the radiators was buckled, a hole was punched into Spektr's hull, and the module began to depressurize. This was not a slow leak - the crew heard a hissing sound and felt their ears pop. They disconnected the power cables leading from Mir to the main station and closed the hatch on the core module transfer section that led to Spektr. The Spektr module became fully depressurized, remaining docked to Mir with its docking hatch open. The loss of electrical connection between Spektr's solar panels and the main station cut the available power supply to the station, crippling its operations until later repairs reconnected the electrical lines. Tsibliev was also the pilot on a previous orbital collision, when he banged Soyuz TM-17 into Mir in Jan 1994. After the return of the crew to earth he was found to be to blame for the incident, although the fines assessed were later dismissed. The Progress M-34 cargo ship was backed to a safe distance from the station and was destroyed in reentry on 2 Jul 1997 06:31:50 GMT. Total free-flight time 9.90 days. Total docked time 76.70 days.

  • 1997 April 7 - Mir News 353: Launch Progress-M34. 

    The Progress-M34 was launched from Baykonur on 6.04.97 at 16.04.05 UTC. This was according to plan. Until now (morning of 7.04.97 UTC) the flight of Progress-M34 is proceeding well. During the 4th and 5th orbit the necessary orbit corrections have been executed. If all will go as planned the Progress-M34 will dock to the aft (Kvant-1) docking port (+X axis) on 8.04.1997 at abt. 1729 UTC.

    Radio traffic Progress-M34: In the evening of 6.04.1997 the transmitters of Progress-M34 could be monitored in the 166, 165 and 922 mc bands between 2039-2042 UTC and 2209-2213 UTC. Radio traffic Mir: During the last nights there has been a lot of radio traffic. The windows during hours in which the crew normally is sleeping were needed badly to co-ordinate with TsUP matters regarding a lot of technical problems.

    Significance of the freighter Progress-M34: These days the Mir-space station goes through a very critical phase. A lot of failures harass the Mir-complex during the last weeks and in particular the problems regarding the maintenance of an acceptable atmosphere on board in fact passed admissible limits. The only way to produce oxygen is the use of the lithium perchlorate cartridges. The crew cannot use the whole available supply of these so called 'shashki' 2 or 3 of which they consume daily. The series of cartridges to which the 'naughty' one belonged and that caused a fire some weeks ago cannot be used. That means that there is only a supply for a few days. Progress-M34 has to deliver the necessary cartridges to ensure the oxygen supply until the docking of Atlantis in her mission STS-84 in May. Atlantis can also bring to Mir a replacement for the Elektron system. By electrolysis the Elektron can generate oxygen from waste water, for instance water distilled from urine. Possibly the Atlantis will also deliver a new Vozdukh, the system to absorb carbonic acid (CO2) from the air on board. This Vozdukh broke down in the night from 3 to 4 April 1997 and could not be repaired. The failure of that Vozdukh was the last one in a long sequence of set-backs. Fate of the Mir-station as a manned complex is hanging by a thread. If the docking of Progress-M34 to the complex fails the crew will have to return to Earth by Soyuz-TM25 within a few days.

    Docking procedure: This time there is still the possibility to execute the approach and docking in the automatic mode by the system Kurs. If the first attempt to dock in this way fails Tsibliyev has to take over and dock Progress-M34 manually by the system TORU. In 1994 the cosmonaut Malenchenko secured the continuation of the manned flights on Mir with the TORU-docking of Progress-M24. Perhaps Tsibliyev will have to take the same responsibility tomorrow. Radio traffic in the evening of 6.04 revealed that among the activities for 7.04 there would be the checking and training with TORU. Altair-2 (23426 - 94082A): During the 'snail-paced' move of this geostationary satellite from East to West she is not operational and will not be used for Mir-TsUP communications. It might be possible that Altair-2 equal to her predecessor Altair-1 has a service beacon on 11.380 GHz. If so we might be able to catch up a sign of life of this satellite before she reaches the position over 16 dgs West. .

    C.M. v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 9 - Mir News 354: Progress-M34. 

    Without problems the freighter Progress-M34 linked up with the Mir-complex. The soft docking, the so called 'kasaniye' (touch) took place on 8.04.97 at 17.30.01 UTC. The approach and docking took place in the automatic mode by the use of the system Kurs. The Progress-M34 docked at the aft (Kvant-1 +X axis) docking port. During the 1st pass of Mir and Progress-M34 (orbits 63618/34) between 1721-1726 UTC it was obvious that the approach was going on. The crew did not report many details of the approach apart from the distance: 150 M. Tsibliyev was on the alert to take over manually by the system TORU, but he met problems with the image on the screen, which he needed for that operation. In co-ordination with TsUP he even consulted the on board documentation to resolve that problem if necessary. So that what I could derive from radio traffic did not convince me that the approach was successful. Moreover LOS for my position was 4 minutes before the actual docking. During the next orbit (63619 - 1856-1903 UTC) it was obvious that the docking had been successfully accomplished: of the 2 hatches between the Kvant-1 and Progress-M34 the crew already had opened the hatch on the side of Mir. They had to wait with the opening of the Progress-M34 hatch until the airseal checks had been completed. The next orbit everything had been opened and the crew already had deployed an air hose between the 2 objects. The mix of the oxygen coming from Progress-M34 with that of Mir did not give any problems.

    Mir-routine: So for the time being the exploitation of the Mir-space station as a manned complex has been secured. Now there are sufficient lithium perchlorate cartridges to ensure the oxygen production until the arrival of Atlantis in May. Progress-M34 delivered a lot of spare parts and reparation material , but whether these are sufficient to do something on the defective Elektron oxygen machines is not sure. Let us hope that there is now enough material to do something on other defective and faltering systems. The failure of the CO2 absorption filter Vozdukh emerged less than a week ago so it is unlikely that the Russians were able to deliver with Progress-M34 anything for the reparation. Apart from the lithium perchlorate cartridges Progress-M34 brought a tank with 50 KG pure oxygen.

    Compliments: The Russians deserve our serious compliments for the fact that they again solved a lot of almost hopeless problems and thus made the continuation of the co-operation with NASA in the IRS Alpha precursor program possible. The history of the Russian people that suffered so much ("mnogostradal'nogo Russkogo naroda") gave the Russians the instinct to survive during the most inclement circumstances and in spaceflight they regularly proved that they know how to use that quality.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 19 - Mir News 355: Mir-routine. 

    Immediately after the opening of the hatches to Progress-M34 the crew began to unload the most important stuff for direct use. They used a part of the new arrived pure oxygen supply and new lithium perchlorate 'disks' for oxygen production. Radio traffic revealed that the cosmonauts without delay had started the repair of the Elektron system in Module-D (Kvant- 2). On 11.04 this Elektron was activated, but after a few minutes during which oxygen was produced it switched itself off. On the days to follow the crew regularly worked on this system and to undo the last failure they even used a part of the unserviceable Elektron in Module-E (Kvant-1).

    The urgent work on the Elektron caused a considerable work overload of the crew. These days the astronaut Linenger is often deployed to assist in this repair work for which he has to refrain from a part of his American experiments. A few times the work on the Elektron had to be suspended for the execution of repair work with a higher priority. This had to do with a lot of leakage in the heating- and cooling circuits in the Base Block and Kvant-1.

    The leaks in the cooling loops in Kvant-1 caused the outflow of cooling liquid (ethylene glycol) and the decrease of the pressure within that circuit. A sufficient cooling is also needed for the functioning of the carbon dioxide (CO2) absorber Vozdukh. For the neutralisation of CO2 in Mir's atmosphere there is another alternative. Progress-M34 delivered for that purpose canisters lithium hydroxide. Meanwhile the Elektron in Module-D and the Vozdukh CO2 scrubber are functioning. The problems with the life support systems on board caused a high humidity and consequently a lot of condensation. Twice a day Tsibliyev can be heard reporting pulse rates, blood pressures, skin temperatures and blood oxygen saturation of all crew members.

    Orbit correction: Using the engines of the Pr-M34 the orbit of the Mir-station had been corrected on 15.04.19997 at 12.46.01 UTC. Apogee and Perigee changed from 397.16/381.63 KM to 402.54/389.51 KM.

    Solar orbit: Within a few days Mir will enter a so called solar orbit. During this period Mir will continuously remain in sunlight. Then it will be more difficult to control the on board temperatures. Tsibliyev said that physically the crew is able to sustain this inconvenience, but that he has some concerns about the equipment of the complex.

    1st Spacewalk (EVA) Mir Main Expedition 23/ NASA 4: This EVA is (or possibly meanwhile: was) on schedule for 29.04.1997. The EVA will be executed if the repair work can be accomplished before a determined deadline.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 25 - Mir News 356: 1st Spacewalk (EVA) Mir 23/NASA 4. 

    Vo chto by to ni stalo. This is the Russian analogue for 'At any cost'. Monitoring radio traffic during the last days I realised that those responsible for this Mir/NASA expedition decided to stick to the EVA on 29.04.97 and this made me use this expression as a sub-title for my report about that EVA. In fact I expected that the long sequence of serious technical problems and consequently the enormous strain for the crew justified the cancellation or at least a suspension of that EVA. Officially has been announced that the situation on board is almost back to normal and that the health condition of Tsibliyev and Linenger is such that they can do that EVA. The EVA is on schedule for 29.04.1997 at 0450 UTC (opening of the hatch) and will last 5 hours and 30 minutes. Using spacesuits of a new design delivered to Mir by the freighter Progress-M34, Tsibliyev and Linenger will install American experiments at the outer surface of Kvant-2 (Module-D) and the SO (the docking compartment at the Kristall (Module-T). They also will retrieve similar experiments which had been installed there in the past. Today the 'spacewalkers' trained for that EVA. In the past the preparations for EVA's started a long time before the planned date en during the last few days crews always fully concentrated on the oncoming EVA. They always got 1 or 2 days off to enable them to start the EVA as fit as possible. This time the preparations started only a few days ago and they had to use a part of the time for maintenance and repair activities. The cosmonauts are very tired and they yearn for a day off. Another problem during this EVA is the communications infrastructure. There is no Luch available. Altair-2 is still moving to the West and not operational at the moment. In the very beginning when there were no geostationary satellites available for Mir-TsUP (or: Salyut - Zarya) communications Russia had a fleet of tracking ships all over the world. Of this fleet only 4 ships are left, 2 of which are operational, but they have to remain in St Petersburg until there are means for exploitation. It is true that TsUP has the possibility to use Dryden and Wallops in the USA and Oberpfaffenhofen in Germany, but that is not enough to fill up all the gaps in the infrastructure. Telemetry monitoring during EVA's is essential. If all goes well Tsibliyev and Linenger can be heard while they are on their way back to the airlock of Module-D during Mir's orbit 63941 between 1000 and 1030 UTC on 29.04.

    During a short interview with an American radio station Linenger on 23.04.1997 told, that they had a rough time, but that they succeeded in restoring the situation almost back to normal and that they all were doing fine. About the leakage of the cooling system in Kvant-1 and the eventual influence of ethylene glycol on the health of the crew he said that the effects in the long run are still unknown.

    Solar orbit: In my MirNEWS.355 I suggested that the next period in which the Mir- complex would remain permanently in the sun was to begin in a 'few' days. This was an error. The next solar-orbit period will be in the first week of June.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 April 29 - EVA Mir EO-23-1.  Spacecraft: Mir.

    Test of new spacesuits. Retrieved and installed external equipment.

  • 1997 April 29 - Mir News 357: 1st Spacewalk (EVA) Mir 23/NASA 4. 

    This EVA passed of successfully and without problems. Tsibliyev and Linenger opened the hatch of the airlock of Kvant-2 on 29.04.1997 at 0510 UTC and closed this after the EVA at 10.08.30 UTC. Duration: 4 hrs 57 mins and 10 secs. The cause of the slight delay is still unknown. The fact that the EVA lasted much shorter than the planned 5 hrs 30 mins was no indication that they had been forced to return earlier but they just accomplished their tasks well within the duration which had been foreseen. These tasks consisted of the installation of the OPM (Optical Properties Monitor) at the outer surface of the SO (docking compartment at the Kristall module). Having this done they moved by the crane Strela to the Kvant-2 where they retrieved the American experiments PIE (Partial Impact Experiment) and the MSE (Mir Sample Experiment). These experiments will be brought back to earth by the Atlantis in May this year. The last task was the installation on Kvant-2 of the Benton Radiation Dosimeter. This instrument will measure the intensity of the radiation between 51.6 dgs North and 51.6 dgs South. The areas between these latitudes will be covered by the IRS, which will orbit in the same inclination (51.6 dgs) as Mir. During the first pass for our location in orbit 63941 (0958- 1010 UTC) the EVA was in its final phase. The both 'space-walkers' already were in the airlock, which they had entered at 0930 UTC. During radio windows they worked with tranquillising music in the background. Radio traffic revealed that Tsibliyev and Linenger had a lot of fun and acted fully relaxed. The EVA was successful and they did not meet any problems. The new type of the Orlan DMA spacesuit was used for the first time and during the pass in orbit 63942 (1133-1145 UTC) Tsibliyev reported his satisfaction about the improvements. He told that his good experience with this spacesuit during training in the hydrolab now has been proven in practice. The suit is very flexible, and especially the gloves are very good: it is much easier to use your fingers. And Tsibliyev has the right to judge this for he did 5 EVA's during his mission in 1993. During the EVA Lazutkin remained on board where he watched the systems, made films of his colleagues, helped them with advice and communications. If the present good luck of the Mir exploration will not vanish Lazutkin will do 2 EVA's together with Tsibliyev during this Mir 23d Main expedition.

    Admiration: All those responsible for the achievements of today: the crew, but also the flight control and consultative groups in Korolyov and Houston deserve our admiration for the way in which they showed their skill and this example of excellent international co-operation. They had the courage to execute this difficult operation just a week after a long period in which the operational life of the Mir space station was hanging by a thread. Let us entrust the work on future space flight projects in their hands!

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 May 11 - Mir News 358: Mir-routine. 

    The successful spacewalk (EVA) gave the crew the elixir they badly needed. In the period after the EVA the lion's share of the activities had to consist of the preparations for the arrival of Atlantis on mission STS-84 on 17.05 (wind and weather permitting). Of course they do a lot in this respect, but repairs and the struggle to restore failing systems almost overtax the cosmonauts.

    They had to replace a number of essential parts of the SRV-U (the system for regenerating water from urine). Also the system SRV-K, to make water from condensation had to be mended. A few days they had to spend a lot of time on the 2 KOB-systems. One of those systems showed a repeatedly pressure decrease. They needed a pressure hose for the repair and tried out some hoses they found. At last they connected one that fitted and solved the problem by the separation of both systems. They postponed the search for the leaks in the KOB-1 and 2 and the cooling loop in Kvant-1 until after the departure of Atlantis.

    For the co-ordination of all activities and to get the necessary advice from TsUP all VHF-windows are needed and used. They also communicate via Dryden and Wallops in the USA and Oberpfaffenhofen in Germany, even during holidays. Sometimes a failure emerges spontaneously during VHF-conversations. For instance 11.05 during the pass in orbit 64127 at 0639 UTC TsUP ordered Tsibliyev to switch off the cycling of the solar panels and when he did so the SOI (possibly the system for orientation and stabilisation) stopped. The reserve system (SOI-2) immediately took over. During the last days special attention had to be paid to the movements- (attitude-) control systems. The external thruster in the Sofora mast (VDU) has been used, possibly to take care for the stabilisation during a reset procedure for the gyrodynes.

    Preparations for the arrival of Atlantis: Especially Jerry Linenger is very busy with the selection and the arrangement of that what he has to deliver on Earth. The Russians also do so with the help of checklists. The main bulk of cargo for return consists of samples and software of experiments, but there is also a lot of defective and used equipment and parts of systems.

    Altair-2: This geostationary satellite (23426 - 94082A) accomplished its walk from 96 dgs East to 17 dgs West, but did not make a stand. To stabilise the satellite over the calculated sub-satellite point (between 16 and 17 dgs West) the VKS (Russian Space Forces) have to correct the orbit such that the period will become 1436 minutes ) on day 128 the period was still 1438 minutes.

    Mission STS-84 Atlantis: The main purpose of this mission is the delivery of Mike Foale and the relief of Jerry Linenger for return to Earth. As soon as Mike Foale's 'seat liner' has been transferred to Mir (in fact via Mir to Soyuz-TM25) Mir mission will get the designation Mir23/NASA5. If, wind and weather permitting, Atlantis will blast off on 15.05 the following schedule can be used: Launch 15.05 at 0808 UTC, opening hatches 17.05 0428 UTC. Undocking 22.05 at 0405 UTC Landing 24.05 at 1153 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 May 15 - STS-84.  Spacecraft: Atlantis. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Atlantis blasted off on a night launch to Mir, docking with the station on May 17 at 02:33 GMT. Jerry Linenger, who had begun his stay on Mir in mid-January aboard STS-81, would return aboard STS-84. Michael Foale would be left at the station for his stint as the American crew member of Mir. The crew transfered to Mir 466 kg of water, 383 kg of U.S. science equipment, 1,251 kg of Russian equipment and supplies, and 178 kg of miscellaneous material. Returned to Earth aboard Atlantis were 406 kg of U.S. science material, 531 kg of Russian logistics material, 14 kg of ESA material and 171 kg of miscellaneous material. Atlantis undocked from Mir at 01:04 GMT on May 22. After passing up its first landing opportunity due to clouds over the landing site, the Shuttle fired its OMS engines on the deorbit burn at 12:33 GMT on May 24. Atlantis landed at 13:27 GMT at Kennedy Space Center's runway 33.

  • 1997 May 24 - Landing of STS-84. 

    STS-84 landed at 13:27 GMT with the crew of Precourt, Collins Eileen, Clervoy, Lu, Noriega, Kondakova and Linenger aboard.

  • 1997 May 25 - Mir News 359: Chronicle. 

    Just before the beginning of Atlantis mission STS-84 I left my 'station' for a badly needed vacation. For those who use my 'MirNEWS-series' as a chronicle I decided to draft a short summary of that mission. The information therein I derived from different sources.

    Atlantis STS-84 mission largely accomplished successfully: Launch Atlantis on 15.05.97; flawless docking with Mir on 17.05.97. Michael Foale relieved his colleague Jerry Linenger. Mir's mission will be named : Mir 23 / NASA 5. Both crews succeeded in transferring mutually all what had to be transferred within the 5-day period. Adding a 6th 'docking day' was not needed.

    Mir was plentifully provided with an extra supply of water and oxygen en the replacement equipment and spare parts to postpone for a very long time the definitive termination of the ageing space station. The most important equipment for that purpose was the new oxygen machine Elektron, which had to be installed in the Module-D (Kvant-2). The old Elektron which had been repaired some weeks ago and has been operational in Module-D has been reinstalled in the former spot in Kvant-1 to be used as a reserve. The delivered supply of oxygen enables the crew to refrain for a long period from the use of the Elektrons. Defective equipment, for instance the old Elektron, which could not be repaired, has been brought back to earth for analysis.

    Originally there has been a plan to deliver a new Antares transmitter for communications via the geostationary Altair-2 (now in position over 16 degrees West). Information about this plan is still unclear and even sometimes contradictory. Communications: During the combined flight the communications also to and from Mir had been handled to a large extent via the American TDRS-facilities. Mir communicated directly with tracking stations on Russian territory using VHF frequencies.

    After the launch of Atlantis on 15.05 Eileen Collins could be heard on 259.7 mc between 0826 and 0829 UTC when she via a tracking station in Spain reported the 'power down of the APU'. Shortly after the stabilisation of Altair-2 over 16 degrees West there has been word that the satellite had a transmitter failure and that the Russians would do all what was possible to reactivate this transmitter. Due to my absence I was not able to monitor 10.830 Ghz.

    During my stay in Budapest I met a 'colleague' and he told me that he received somewhat like a 'wide band' signal on that frequency, probably a test signal by the VKS (Russian space forces). This was on 19.05. Later on and until the afternoon of 21.05 the transponder transmitted a continuous carrier without modulation. Another colleague in Western Europe monitored the wideband signal and recorded this. Meanwhile there came some information about the Antares transmitter on board Mir.

    The installation of a new Antares has been put back until the arrival of a needed part which has to be delivered by Progress-M35 (launch 22.06, docking 24.06). Conclusion: Altair-2 is operational. The problem is still on board Mir. Mir-routine: The 3 crew members on board Mir again have to do the job alone. Just before the arrival of Atlantis they repaired the defective water regeneration systems (SRV-K condensation and SRV-U urine) .

    Before a profound analysis on Earth of the quality of the water regenerated by the SRV-K they are not allowed to drink this water. They are satisfied about the new supply of oxygen and the relative high pressure of the atmosphere on board: 780 mm. One of the first priorities is the search and elimination of a leakage in the cooling loop VGK.

    The passes of the Mir-station for our position take place during the night hours. So for a short period there will be not much radio traffic via VHF unless something special happens during these night hours. I will remain on the alert!

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 12 - Mir News 360: Progress-M35. 

    This freighter is on schedule for late this month. If launch and flight will go as planned Progress-M34 will have to leave the aft docking port (+X-axis) the day before the arrival of Progress-M35. Apart from the normal cargo a badly needed component for the Antares-transmitter on board Mir has to be delivered by Progress-M35. Until the restoration of Mir's satellite relay system audio and video downlinks will be limited to ground station passes.

    Progress-M34: It might be possible that before the departure for decay in the Earth's atmosphere the Russians will execute an autonomous flight with the old freighter to test the TORU system. Thus far no confirmation about this operation. Radio-amateurism: The fact that the Mir-crew is active again on the radio-amateur-frequencies confirms that the situation on board though not fully back to normal, improved to such a degree that they got more time to relax.

    During almost every pass within our range the amateur station in the 145 mc band is active, mostly in Packet Radio, but also in Phone. Mike Foale (call KB5UAC) or the Russians (R0Mir) can be heard on Mir's downlink 145.800 mc. (uplink 145.200 mc). The crew transmitted a P/R message in which they said that they planned to increase P/R traffic. In another P/R message they reported that the Safex-2 transponder in the Priroda Module is operational again. Downlink is 437.950 mc, uplink 435.750 mc. To open the transponder a CTCSS tone of 141.3 hertz is needed. During docking operations with Soyuz-TM- and Progress-M ships and Shuttles Safex-2 will be OFF to avoid interference on crucial systems.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 16 - Mir News 361: Progress-M35. 

    If all goes according to plan this freighter will be launched on 27.06.1997 at 0630 UTC. If launch and flight will be successful Progress-M35 will dock at Mir's aft docking port (X-axis) on 29.06.1997 at abt 0748 UTC.

    Progress-M34:

    There are no plans for an autonomous flight with Progress-M34. If during the first day of the flight of Progress-M35 all goes well Progress-M34 will separate from Mir on 28.06.1997 and brought on a destruction course for decay over a designated area in the Pacific East of New Zealand.

    Radio-amateur traffic:

    As requested by radio-amateurs in the USA the 'downlink frequency' of the VHF station in Mir's base block has been changed from 145.800 to 145.985 mc. This change took place on 15.06.97. Almost during every pass within our range traffic, mainly Packet Radio, can be monitored. During the last days Foale could be heard in Phone. Foale is a skilled radio-amateur with a very good memory. During a QSO with the Belgian amateur ON6GP he remarked that during mission STS-45 ON6GP spoke with Foale's crew mate the Belgian astronaut Frimaut.

    Communications:

    Tsibliyev and Lazutkin during every pass discuss their reparation activities. They meet a lot of problems with cables and contacts which they cannot find or do not fit. Undoubtedly the present mission, teased by a lot of problems and set-backs, is leaving its traces on the psychological stamina of Tsibliyev and Lazutkin. Especially for Tsibliyev it is not always easy to maintain his normal flexibility.

    In a long conversation with his father Foale told that he just flew over England. The British isles were fully overcast and the cloud layer had the same shape as the country itself. He also told that Tsibliyev and Lazutkin badly hope that the relief crew will be launched at abt. 8.08.97. The Russians will be relieved by Solovyov and Vinogradov. After the departure of the present crew Foale will remain on board Mir. So he will be a member of Mir's Main Expedition nr. 24 (Solovyov and Vinogradov) for a period of appr. 7 weeks. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 25 - Mir News 362: Progress-M34. 

    In contradiction to the information given in my MirNEWS.361 the Russians decided to execute manoeuvres with this old freighter for tests of the TORU system (system for remote controlled

    guidance from inside Mir). The fact that departing Progress-M-ships could be used for that purpose had been announced, but I could not get confirmation about the possible use of Progress-M34. Radio traffic during the last days revealed that Tsibliyev had got orders to check the TORU-system during an autonomous flight of Progress-M34. He and Lazutkin repaired electronics of the TORU and TsUP told Tsibliyev what he had to do. The manoeuvres should be executed during those periods in which Mir would be in range of ground stations.

    Progress-M34

    undocked from Mir on 24.06.97 at 10.22.50 UTC. Just after undocking Progress-M34 flew above the Mir-complex and a few hours later Tsibliyev reported that Progress-M34 flew behind Mir in a distance of appr. 2 KM. Progress-M34 had to be redocked at Mir with the use of the system TORU on 25.06.1997 between 0920 and 0925 UTC. THIS DOCKING ATTEMPT FAILED. When this report 'went to press' specialists at TsUP were analysing the situation and whether or not -and if so when- a second attempt would be made had not been decided yet.

    Progress-M35:

    The launch of this freighter is on schedule for 27.06.1997 at 0721 UTC. If this launch will take place (in view of the situation with Progress-M34 might this been changed) and if all goes according to plan this freighter will have to dock at Mir aft (+X-axis) port on 29.06.1997 at 0848 UTC. (In my MirNEWS.361 the estimated times were incorrect. I mixed up DMV time (TsUP time) with Moscow summer time.)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 26 - Mir News 363: The following message received from VideoCosmos. 

    Co redistributed by Chris v.d.Berg under MirNEWS.363 and MirNWS.363 (no Dutch translation available yet due to lack of time)

    Subject: Emergency on Mir

    Novosti Kosmonavtiki June 25, 1997 -- Moscow, Russia -- Progress M-34 cargo vehicle collided With the Spektr module of Mir space station earlier today but the crew survived. The collision occurred before 09:18 UTC during Progress' fly around in remote control mode before scheduled re-docking. The crew haven't had communications with Russian ground stations at the time. The cargo spacecraft sheared a half of Spektr solar panel and made damage to the module itself. Depressurization of the station had begun but the crew succeeded in fast closing the hatch to Spektr. The rest of the station is being re-pressurised. Also, thermal control radiators on Spektr were damaged. There is no immediate danger to the crew but emergency landing is a possible decision. This report is not copyrighted. If you plan to use or publish the report please keep reference to VideoCosmos Co. of Moscow, Russia, and Novosti Kosmonavtiki Magazine.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 27 - Mir News 364: Progress-M34. 

    The Russians abandoned the plan to finish the existence of this freighter today. Progress-M34 is still needed for Telemetry analyses, necessary for the investigations on the cause of the 'mini-catastrophe. For the time being it is extremely difficult to get a reliable picture of that what happened due to the huge amount of versions and rumours about the failed docking attempt. When Progress-M34 will enter the earth's atmosphere and decay has been not decided, it might take place on 28 or 29.07.97.

    Inquiries: An extensive commission under the chairmanship of the Head of the RKA (Russian Space Agency), Yuriy Koptev, discussed the situation on 26.07.97 and decided to delegate the investigations to one or more working groups. These specialists will pay extensive attention to the Telemetry from Progress-M34 after the undocking until the collision. Already before the session of the commission Koptev gave a statement in which he emphasised that the operations with Mir will not be interrupted, that the crew will not be evacuated and that Russia will perform her obligations in the framework of the international co-operation. (How far political intentions will conflict with technical imperfections and even impossibilities certainly will turn out in due course.)

    Intentions and options known up to now (27.06.1997 1200 UTC): A lot of press-releases speak about the necessity to make a spacewalk (EVA) for the inspection and eventual repair of the little gap or crack in the hull of Module Spektr. Such an EVA will certainly be executed, but this will take place not before the arrival of the next cargo ship Progress-M35. The first EVA will be a so called 'internal EVA' using the transition section (P.Kh.O.) as an airlock via which the cosmonauts can enter the Spektr.

    Module Spektr: For a long time this module was the 'base and home' of the American astronauts. In this module Foale disposed about a lot of equipment and experiments. The crew has to determine what still is available and can be saved and what is lost. For the time being a lot of experiments cannot be executed and in fact the experimental program for this expedition is almost fully suspended. One of the 4 solar panels of Spektr has been severely damaged, possibly beyond repair. The other 3 might be able to deliver power, but due the disconnection of cables, some of those cables had even to be cut in two, they are out of order. The damaged one and one of the other 3 are badly needed for power supply for the whole complex. The event caused a power reduction of appr. 50% . Before I spoke about a little gap or crack and not as generally is done in publications about this damage, about a gap, or even big hole. If it would be a real gap the crew would be dead. Depressurization would have been a matter of seconds not only or the Spektr but also for the whole complex. This depressurization was in fact a process which passed off slowly. The crew felt the decrease of the pressure in their ears and they had still enough time to close one of the hatches to Spektr and -possibly we will hear about this later- do a lot of things before closing that hatch.

    Situation on board of Mir : A summary about the developments after the collision as derived from the enormous amount of radio traffic will be published in NEWS.365.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 June 28 - Mir News 365: Radio traffic after collision Progress-M34 with MIR.. 

    On 25.06.1997 during the first pass of the daily sequence (orb. 64831, 1049-1054 UTC) it was obvious that something went terribly wrong. If the redocking would have been a success this should have been obvious during this traffic. No word about the Progress-M34. The only subjects about which the crew spoke with TsUP were the systems on board Mir. In the first place they had problems with the SUD (attitude control) and something had happened with a module. TsUP transmitted a long series of 4-digit groups and the crew got orders to record and to collate them ('kvitantsiya').

    In the next pass (orb. 64832, 1223-1232 UTC) reports about serious problems indicating that the complex had suffered from a heavy blow. An emergency signal warned that the power supply was too low (tension too low), that storage accumulators could not be charged and that the attitude of the complex had been changed and flew on its side. One or more of the 5 still available solar arrays could not be adjusted for a good angle towards the sun.. Tsibliyev reported that they were unable to change this and that the complex had a movement along the X-axis.

    The crew got orders to activate the direct TV-link (commands Anna-72 and Anna-86) and to send images. Mike Foale made this images with a camera. (These images could be seen all over the world during the rest of the day). Very alarming was that what the crew reported during the 3d pass (orbit 64833, 1359-1409 UTC). Those solar panels which were still available could not be adjusted via computer commands, but this had to be done manually by the cosmonauts.

    The gyrodynes did not work any more , the electrical tension was too low and the Ts.V.M.-1 (the main computer) ceased to function. The SUD failed and this was also the case with such a system in Module-D. After reporting all these calamities Tsibliyev stated that the situation was very bad. A number of ventilators did not work and the crew was grateful about the fact that the ventilators in Module-D functioned normally.

    The fact that the gyrodynes stopped and did not consume power anymore decreased the burden on the power supply. After a long discussion about the power problems the crew got permission to adjust the solar panels of Module-D manually for a better angle towards the sun. In the background the voice of the veteran cosmonaut Vladimir Solovyov, Head of Flight Control, could be heard. As much as necessary the crew could use the Soyuz-TM25 and in case of a failure of the communications from the Base block they could use the transceiver of that ship.

    The traffic during the 4th pass (orb. 68434, 1535-1546 UTC) began with the cheerful voice of Foale asking Tsibliyev how he felt himself. Tsibliyev said that he was very tired and suffered from strain caused by the event. Before LOS TsUP gave the windows for communications via the ground facilities of Oberpfaffenhofen, Dryden en Wallops in the coming night.

    There was also good news: Foale reported that the amount of CO2 in the air was so low that the CO2 scrubber Vozdukh was not needed. An inconvenience was the fact that the alarm light : 'Depressurization of the complex' was burning continuously and that reset was impossible while the mano-vacuummeters indicated that the pressure remained stable (692 mm). During a following pass Tsibliyev said that he understood that the launch of the Progress-M35 had been put back. TsUP confirmed this. (to be continued)

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 1 - Mir News 366: Radio traffic in the period 26.6 - 1.7.1997. 

    During this period it was for me a relief when I during the first pass of the daily sequence heard the voices of the crew. Every conversation between the crew and TsUP referred to the difficult situation and their 'struggle for life'. 26.06: Just like on 'collision day' they again had to do everything to adjust those solar-arrays which still were operational to the best angle towards the sun.

    The absence of the gyrodynes for the movements control and the absence of the possibility to have commands executed by computer programs means that the crew has to adjust the solar arrays manually. One of the complaints was that the solar arrays on Module D moved very slowly. Nevertheless the angles towards the sun gradually improved leading to an increase of power supply. The crew did all what was possible to determine the damage by observations and making images via several portholes, but it was impossible to get a full picture.

    For the reception of radiograms the RTTY system was in use again. The attitude control of the complex was executed by thruster jets, also with those of the transport vehicle Soyuz-TM25. They did not do any experiments for which electrical energy was needed and all radio-amateur activities had been suspended. For the filtering of the air from CO2 now and then the Vozdukh scrubber was activated.

    27.06: This day there was word about a gyro-stabilised orientation, possibly with the attitude control of the Soyuz-TM25. For the neutralisation of CO2 TsUP wished the use of lithium hydroxide canisters. Tsibliyev asked permission to do this with Vozdukh. At first they had to do this with those canisters, but later on they got permission to switch on Vozdukh for a while. The crew also worked on the Elektron, but this oxygen producer had to remain switched off to economise energy. During the pass in orb. 64863 there has been a TV-link (Anna-72 and Anna-86) and possibly they used for the phone during these communications the VHF-2 130.165 mc.

    During the pass in orb. 64865 the crew answered questions of a lady on earth. The crew said that only a few experiments ('sleep' and the 'orangery') can be executed. During this interview the possibility of a spacewalk (EVA) was mentioned. Tsibliyev spoke about an 'internal' EVA. Tsibliyev hoped that their spacesuits will enable them to enter the Spektr. He stated that the present situation is far from hopeless. Problem is that 1 solar array has been severely damaged. The other 3 solar arrays on Spektr are still in good order, but it is a 'bloody shame' that they cannot deliver electrical power. One of those 3 is badly needed for the power supply.

    The lady asked how things are looking inside the Spektr. Tsibliyev said, that they do not know this for they have not been inside. In his opinion a space station can be compared with a 'test firing range' where everything is possible. They are very proud of their Mir. Cosmonauts are prepared to undergo normal and emergency situations, even those which have not been foreseen. But together with the experts on earth they always will 'twist themselves out'.

    28.06: Today again attitude corrections with the thrusters of Soyuz-TM25. Also a few times TV-links. The work on the Elektron has been postponed until next Monday, probably due to a valve that cannot be opened. Later on they spoke about the functioning of the Elektron in Kvant. (37KE). Today the transfer of radiograms with Packet Radio could be monitored. A lot conversations about the 'internal' EVA. The equipment needed for this EVA has to be transferred from the Sh.S.O. (airlock of Module-D) to the P.Kh.O. (transition section, which again has to function as airlock). They spoke about the spacesuits, POV, BSS and so on.

    29.06: During passes they almost exclusively spoke about the next EVA and also mentioned the spacesuits which have to be used: Orlan-M or Orlan-DMA. Foale is also involved in the solution of these problems. It was also obvious that a part of the available gyrodynes is functioning normally. Now and then they speak about the switching off of one gyrodyne or the use of a reserve.

    30.06: Again a lot about the EVA. There was also work to do on the cooling loops VGK and K.Okh-B in Kvant (37KE).

    1.07: Foale spoke with Wendy Lawrence, his successor. He says that his 'little room is in vacuum now'. Meanwhile the radio-amateur Packet Radio transmissions on 145.985 mc have been resumed. (this means that the power supply situation really improved) During the pass in Orb. 64925 Tsibliyev reports: 'At about 1100 UTC we heard some dull claps or knocks. It was not clear what it was. When we at 1103 UTC entered the light from the shadow we saw a big cloud of very little white flakes near the Module-O (Spektr). Obviously there is fuel leaking away from somewhere'. He asked TsUP to check the fuel tanks by Telemetry.

    That's all for now folks.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 2 - Mir News 367: Progress-M34. 

    This naughty boy (or is it girl?) ceased its existence on 2.07.97 at 06.32.00 UTC. Progress-M34 burnt up over a designated area in the Pacific East of New Zeeland. During the autonomous flight until decay specialists used Progress-M34 for tests in the framework of the investigations in the cause of the fatal event on 25.06.1997.

    Progress-M35:

    The launch of this new freighter with a partly replaced cargo is on schedule for 5.07.1997 at 04.11.54 UTC. If all goes according to plan the Progress-M35 has to link up with Mir's aft (+X) docking port on 7.07.1997 at 05.58.15 UTC.

    Cargo of Progress-M35:

    The original cargo has been partly replaced by equipment needed for the activities in relation to the Module Spektr during an internal spacewalk . With Progress-M35 an Antares transceiver for communications between Mir and TsUP via the geostationary satellite Altair-2 over 16 dgs West will be brought to Mir.

    The mysterious white flakes:

    After MirNEWS.366 went to the 'press' there was still a pass of Mir in orb. 64927 in which Lazutkin reported that they did not see those flakes after their first observation.

    Morale on board Mir:

    The morale is excellent. Tsibliyev regained his old flexibility and he is very busy with the very complicated preparations for the internal EVA (so in fact an IVA) which possibly will be executed in the night from 11 to 12.07.1997.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 5 - Progress M-35.  Spacecraft: Progress M. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 7 Jul 1997 05:59:24 GMT. Undocked on 6 Aug 1997 11:46:45 GMT. Redocked with Mir on 18 Aug 1997 12:52:48 GMT. Final undocking on 7 Oct 1997 12:03:49 GMT. Destroyed in reentry on 7 Oct 1997 17:23:00 GMT. Total free-flight time 2.30 days. Total docked time 80.21 days.

  • 1997 July 7 - Mir News 368: Progress-M35. 

    The start of this cargo ship from Baykonur took place on 5.07.97 at 04.11.54 UTC. During the pass in orb. 2, 0847-850 UTC, the Telemetry transmissions in the 166 and 165 mc could be heard and during the pass in the next orbit these transmissions, but also those of the beacon in the 922.755mc could be monitored. On 6.07.1997 during the passes in the orbits 18, 19 and 20 good signals on all frequencies and with the doppler shift on 922.755 mc 2 times TCA's could be determined: 071751 and 085100 UTC.

    Progress-M35, approach and docking: Again all went of old: a stable and reliable execution of this operation by the automatic system Kurs. The docking took place on 7.07.1997 at 05.59.24 UTC. During Mir's orbit 65015 from 0549-0554 UTC the approach was going on. At AOS the Progress-M35 was in a distance of 147 M. Tsibliyev reported very little deviations in the course and attitude of Progress-M35. There was a stable GSO (gyrostabilised orientation) and all went so successful that Tsibliyev could load some date, given him by TsUP, in a computer. Just before LOS the distance was still 120 M and the approach was continued with a speed of 30 cm\sec.

    During the next passes they did not speak about the opening of the hatches to Progress-M35. The main subject was the good functioning of the gyrodynes, the good attitude of the complex and the fact that the solar arrays had been turned to a good angle in relation to the sun. The accumulators could be fully charged. The crew has to remove temporarily the spacesuits from the P.Kh.O. (transition section) to get more room for the transfer of goods from Progress-M35 to the rest of the complex.

    The Russians deserve a heartfelt 'Molodtsy' (well done fine fellows). But please let those responsible for Russian manned spaceflight as soon as possible make a deal with the Ukrainian factory Khartron for the restoration of the delivery of the system Kurs. In that way docking-operations can be executed with a 99.99% reliability!! Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 11 - Mir News 369: Progress-M35. 

    In contrast with the normal practice after dockings this time the crew had to wait with the opening of the hatches until the next day to conserve power and to enable the crew to have a good night's rest. The subjects discussed during radio communications in the passes in the first 3 orbits after the docking had nothing to do with the arrival of the Progress-M. They spoke about the replacement of water tanks, the switching on and off of the Elektron for oxygen production and the work on the accumulators.

    They had problems with the BKV-3 (air conditioning) and something was wrong with the Vozdukh, the CO2 scrubber. The next day the crew got permission to open the hatches and to start the unloading and loading of the freighter. They immediately began to pump water into the tanks of the complex. Foale had seen his 'goodies' for which he had been anxiously waiting, but due to the congestion of goods he could not yet reach them.

    This week radio traffic revealed circumstances which did not get much attention in the press and status reports. Everybody is aware of the fact that the module Spektr is as dead as a doornail, but the power shortage also paralysed another 2 huge modules, i.e. Kristall and Priroda.

    Greatest anxieties causes the module Kristall. Near the docking device for the Space shuttle (the SO, docking compartment is attached at the Kristall) the high humidity causes a lot of condensation and there but also in other places Foale and Lazutkin try to absorb this water as much as possible using towels. Foale reported that the temperature in Kristall is abt 4 a 5 degrees Celsius. Tsibliyev told TsUP that he blew air into Kristall for warming up.

    The most important subject remained the preparations for the coming spacewalk (IVA). The lion's share of this work is in the hands of Tsibliyev. When this report went to press there was not yet a complete scenario for the IVA. This meant that Tsibliyev regularly has been confronted with changes. This also in relation to the equipment and tools which they must have at hand during the IVA. Tsibliyev asked for a definitive list of all what has to be put in the IVA bag. Thus far he several times had to replace things. He also urged TsUP to avoid unnecessary delays.

    Now and then TsUP and the crew discuss the collision. Foale and Tsibliyev repeat much what they have told earlier. TsUP is still trying to trace the spot where Spektr's hull has been perforated. TsUP asked Lazutkin to give his opinion based on that what he heard during the collision. He told where he heard the hissing (or: sizzling, Russian word 'shipeniye'). When you should enter the module this must be in the wall on the left hand side. At first the blow was at the radiator, which is installed between the 2d and 3d plane. In the nearest (seen from the place where Lazutkin was) 'quarter'. If that is the place of the fixation at the suspension obviously the puncture must be there.

    Radio-amateurism:

    The Packet Radio 'circular saw rattles' can be heard again on 145.985 mc. Now and then Foale (KB5UAC) publishes by P/R small status reports. For instance: On docking day: 'Progress docked normally this morning. We are waiting 3 orbits before we start to unload it, checking the integrity of the hatch seals. (In fact they had to put this back until the next morning) The station attitude controls system is working well, using the gyrodynes, and the power STH (?) the base block and module Kvant 2 powered (airlock and toilet) with modules Kristall and Priroda unpowered. Greenhouse experiment is continuing, using power from the base block, to dry the seed pods that have formed quite nicely.' After collision day: Our packet pwr supply failed, and we had to rewire the equipment to a newer one. All previous msgs here were lost. TNC Paccomm no longer holds its parameters, if pwr is turned off, since the Progress collision. Mike, KB5UAC.'

    And today:

    'The crew is now extremely busy, trying to crawl through all the bags unloaded from Progress, which are now stored in dark, wet modules, which have no power. We are trying to inventory and assemble the 30 or so cables and adapt, required to install the hatch umbilical. A training run will be done on the 15th and the real EVA sometime after that. I will get some refresher training on preparing the Soyuz for evacuation, and will be in a spacesuit, b, in the Soyuz during the EVA itself.'

    Foale:

    During the period just after the collision Foale had his quarters in the P.Kh.O. (transition section). This P.Kh.O. will serve as airlock during the IVA and so Foale had to remove. He is now living in the module Kvant-2 (Module-D), which certainly will be more comfortable than the P.Kh.O.

    Attitude control:

    During this week the gyrodynes did not function continuously: sometimes all of them of just 1 were spun down for power conservation and in these periods for attitude control the small thruster jets of Mir and (now) the Progress-M35 are used. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 15 - Mir News 370: Spacewalk (IVA). 

    The preparations for the internal EVA were still going on successfully (as far as this can be ascertained by monitoring) when Tsibliyev reported that he had hearth rhythm problems. Initially he discussed this with a doctor, first name Irina, who was not able to diagnose the case and so she did not prescribe medicine. Later on Tsibliyev asked for permission to swallow a pill and for an answer on his question whether he would be able to do the difficult IVA or not. The problem emerged yesterday and now it is known that higher 'doctors' are trying to find a solution. During radio conversations in the passes of orb. 65141 and 65142 it was obvious that the complaints of Tsibliyev will effect further plans.

    The exercise which was on schedule for today (using Kvant-2 to imitate the IVA into Spektr) had been put back and that this was also the case with the IVA itself. Today Tsibliyev declared that if he could have a week to recover and nothing special would occur he wished to do the IVA himself. From the beginning, for instance during the collision , he was so involved in this all that he considers this as his duty. TsUP obviously had other ideas and asked Foale to take the microphone. Foale stated that he had no objections and that he would be very pleased to accomplish this task. He was sure that Tsibliyev would give him the right instructions. Tsibliyev possibly agreed with the possibility that Foale would replace him.

    Foale added that he already knows how to handle the spacesuit Orlan-DMA. Tsibliyev said that the spacesuits were ready for the operation. A few orbits later Mir communicated with TsUP via Altair-2 in phone, but they also exchanged images. For a long time the cosmonauts were in the P.Kh.O (transition section) involved in technical preparations for the IVA. Tsibliyev was the most active crew member during these preparations and did not show signs that he had health- or stress problems. Probably he wants to recapture his place as spacewalker nr. 1. Whether Tsibliyev or Foale will do the IVA is not yet known. The IVA has been put back abt 10 days. Foale did not participate in the discussions from the P.Kh.O. Now and then, but not often, Lazutkin could be heard.

    Altair-2:

    The crew succeeded in restoring the communications from and to Mir via this geostationary satellite. Initially they had problems with their phone during the transmission of TV-images. On Sunday (13.07) they showed little papers with that what they wanted to tell their relatives and friends. On 14.07 they adjusted the installation in which Foale substantially participated. Today, 15.07, the so called Ku-band was fully in use during some passes. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 20 - Mir News 371: Cable trouble. 

    By accident one member of the Mir crew disconnected a cable connection between a rate-sensor in Module Kristall and the SUD (attitude control computer), which caused a troublesome chain reaction of system failures. Among the systems which did not work anymore were also transmitters in the base block, the UKW-1 transceiver and Telemetry transceivers. So for communications, but also for an alternative attitude control the crew had to use the systems of the fully autonomous Soyuz-TM25.

    During the night hours I use to record transmissions using a time switch. In the morning I did not find anything on my tape and during the pass in orbit 65171, 0548-0559 UTC, the 143.625, 145.985 and the 166/165 mc telemetry transmitters did not show any sign of life. I checked whether they used Altair-2 or not: again negative. A few minutes after the pass Geoff Perry told me that he had heard them on 121.750 mc.

    During the next pass they still used the 121.750 mc during which Geoff Perry heard them laughing in reaction on that what TsUP had said. The first pass in which the 143.625 mc was in use again was during orbit 65173 at 0900 UTC. Tsibliyev reported that there has been some recharging of the accumulators again and consequently they had switched on some systems, i.e. the UKW-1 transmitter and Telemetry transceivers.

    In the early morning of 18.07 I was on duty during the nightly passes. During 2 of them (in orb. 65184 and 65185) all service frequencies remained silent, but I had a hope that conditions had improved for on 145.985 mc there were Packet Radio bursts again. During the pass in orb. 65186 Tsibliyev kept watch in the Base Block and he confirmed that the situation was better than the day before. His 2 colleagues still slept which they badly needed because of the fact, as Tsibliyev stated, they had to endure so much during the last days. During the passes still to follow he also slept and the only sign of life was the continuous rattle of Packet Radio. My oscilloscope did not give any indication that Altair-2's downlink was active.

    VHF:

    The first windows in which VHF-traffic could be monitored here before the early morning hours of 19.07 and as my body was longing for a good night's rest I adjusted my time switch so that during all windows a recorder was active. And of course this time not only for the 143.625 , but also for the 121.750 mc. After a night in which I slept like a log I found a recording of the transmissions on 143.625 mc during the first pass in orb. 65199 (0045 UTC). Lazutkin had the middle watch in the Base Block and he reported good results of the recharging of accumulators and the fact that there was GSO-1 (gyro stabilised orientation), a very slow rotation and the complex flew on one side. Later on Lazutkin was in his couch and only the Packet Radio and Telemetry transmitters were active.

    Altair-2:

    During orbit 65203 Altair-2 showed up again. A signal on 10.825 GHz and on the monitor images of floating cosmonauts, the interior of the Base Block and now and then a glimpse of the damaged Spektr. Also phone in which Foale told that he has to use a list with things he needs for the IVA and components for the Orlan-DMA suit. This list in Russian and he asks for an English translation to make it easier for him in contacts with American experts during training for the IVA and the IVA itself. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 22 - Mir News 372: Decisions taken. 

    The present crew has been relieved from the task to do the IVA. The announcement was published on 21.07, but contacts between Mir and Earth, for instance in a conversation between Foale and Frank Culbertson made this clear. Another indication was the fact that the preparations for the IVA had been suspended. Foale said that he was a little disappointed for he personally was hoping to do that work, but he thinks it is the right decision politically but also for this crew. Solovyov and Vinogradov will be launched on 5.08 and dock on 7.8.97. Then the present crew has just a week for the transfer of the station. They will return on 14.08.97 in their Soyuz-TM25. At first Foale did not know what to do with himself when he heard of the postponement, but they have been so very busy in the last 2 months that it is good to have some rest and the possibility to get back to the routines.

    Science:

    Foale's opinion is that his role is changed, for he is there no longer for science, but to help them and to learn and whatever. He values the recent experience. Without the power on the modules you cannot say you are doing active science. If you under these circumstances are saying you are doing the science you would not be telling the truth. He will do all what is possible, for instance with the greenhouse and he will be very busy with towels to absorb condensation water from the walls in the modules.

    Eyharts:

    This French spacionaute will not join the crew of M.E. 24. It would have been senseless, but also irresponsible. He will get the opportunity to fly with a later expedition.

    IVA:

    This operation will take place not before 20.08. Before the IVA Solovyov, Vinogradov and Foale will make an autonomous flight with the Soyuz-TM26 to redock this ship from the aft port (+X-axis) to the P.Kh.O. port (-X-axis). During the IVA Foale will be in the Descent Module of Soyuz-TM26 to activate the BO (life compartment) of that ship as an airlock if Solovyov and Vinogradov cannot get airseal in the P.Kh.O. for instance if the new hatch to Spektr is not airtight.

    Altair-2:

    After the restoration of the power situation of the day before the accident with a computer contact. Altair-2 has been used for TV-contacts, phone, data transmissions and the exchange of service radiograms with Packet Radio.

    Radio-amateur activities:

    Foale has now time to speak with radio-amateurs via 145.985 mc. He made also contacts with some European amateurs. Via Packet Radio he issued the following status report: Subject: Status: I am having frequent power problems with tnc, and loosing all msgs. Sorry. No supply store is near at hand. I would do anything for a 9 pin serial adapter. Getting ready for next crew, August 7th Mike, KB5UAC. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 28 - Mir News 373: Routine. 

    After the announcement of the postponement of the IVA the whole crew showed a great disappointment that they would not do that. But immediately it was obvious that the mood on board was much better. Though 10 days ago they energetically and skilfully worked on the IVA preparations they possibly shrank from the task itself. Many Americans expressed concern about the question what the crew would have to do during the period until their relief. Apparently they thought there on would be an idling bunch of cosmonauts on board.

    This is not true at all: Foale immediately started to fulfil that part of the experimental program for which he does not need the Spektr module: the greenhouse, the study of crystal structures, the beetle experiment and earth observations. And he himself is there: he can continue medical and psychological experiments. He told his American colleagues that the cooled modules Kristall and Priroda attract moisture from the rest of the complex and that the greatest condensation appears in these modules.

    Tsibliyev and Lazutkin are now able to concentrate on the preparations for their return and to continue in a more relaxed way maintenance- and repair work of the life support systems.

    Using air ducts and ventilators Lazutkin blew warm air into the Priroda module and dried this module as much as possible. In a conversation with Mark at TsUP Foale praised Lazutkin for that what he had achieved. The drying of the Priroda made it possible to use it to stow away the hard- and software for the French Pegase expedition and for material and spare parts for the life systems of the complex. Tsibliyev is again fully in command and presents himself in the way I still remember from his flight in 1993/94.

    Altair-2:

    This geostationary satellite is in use regularly , more than Altair-1 in the past, but in view of the fact that 16 windows a day might be possible, they use this possibility relatively seldom. Altair-2 enables the crew to have longer conversations with controllers and experts on Earth. Especially Foale extensively uses this opportunity. The satellite is also in use for the exchange of video images and data to Earth. Obviously the use of the transceiver on board for these communications is limited due to cooling demands. The transceiver and the Elektron have the same cooling loop. Not always the full window for communications via Altair-2 is used. This was the case on 27 and 28.07.

    Cable disconnection:

    It is still unknown who is to blame for this incident. The incident took place during a training for the IVA. During the real IVA this cable has to be disconnected to make it possible to close the hatch between Kristall and the P.Kh.O. So this disconnection must have been mentioned in the timetable for the IVA. I wonder whether or not there was anybody in TsUP who had to monitor the activities of the crew and to warn them not to disconnect that cable, because this was an exercise and not the real thing. Head of Flight Control Solovyov shouted: 'This is not a kindergarten'. Whom did he cry to: the crew or the people with him on Earth? Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 July 31 - Mir News 374: Soyuz-TM26. 

    The launch of this ship with on board a crew of 2 for Mir's Main Expedition 24 is still planned for 5.08.1997 at 1535 UTC and if launch and flight go according to plan the docking will take place on 7.08.1997 at 1723 UTC. This time deviates from the normal routine to dock only a few minutes after LOS for the first pass for our position. This time the docking will take place almost 20 minutes later possibly to enable Solovyov and Vinogradov to make a video and/or photo survey of the module Spektr for damage assessment and to see whether Spektr is not the only module that suffered from the blow on 25.06.97. Recently there have been suggestions that there might be more damage than had been supposed initially.

    On 6.08.1997, so 1 day after launch of Soyuz-TM26 the freighter Progress-M35, meanwhile fully loaded with trash , will leave the aft (Kvant +X axis) docking port for a 10 days lasting autonomous flight. On 7.08 Soyuz-TM26 has to dock at that port, but after the departure of Soyuz-TM25 with the relieved crew on 14.08.97, Soyuz-TM26 with on board Solovyov, Vinogradov and Foale have to redock at the forward (P.Kh.O. = -X axis) port as soon as possible. This is scheduled for 15.08.97. They can fly around, but also wait until the Mir complex has made a turn of 180 degrees around the Z-axis.

    After redocking the Russians have to accept another challenge for already on 16.08.97 Progress-M35 has to redock at the aft (+ X axis) port. This time again in the automatic mode with the reliable system Kurs. There will be no time to recover from the sustained strain for the crew will have to deal with the preparations for the IVA on 20.08.97. If this IVA will be awarded by success TsUP can give green light for an EVA (so a real external one) on 3.09.97 for an inspection of the outer surface of Spektr.

    Radio-amateur traffic:

    On 145.985 mc Packet Radio could be monitored in which Foale gave the following Mir-status report: TNC frozen again, this time the PMS. Waiting for a replacement with Mir 24, Anatoliy and Pavel, docking on the 7th. Crew is preparing for their arrival, getting Progress loaded with trash, to be undocked before next crew. Greenhousing, but not yet showing cotyledons. Mike. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 5 - Soyuz TM-26.  Spacecraft: Soyuz TM. Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Mir Expedition EO-24. The Soyuz docked manually at 17:02 GMT August 7. Over the next six months the crew undertook seven internal and external spacewalks to repair the crippled space station.

  • 1997 August 6 - Mir News 375: Soyuz-TM26. 

    The perfect launch took place on 5.08.1997 at 15.35.59 UTC. On board the crew for the 24th Main Exp. to Mir, Anatoliy Solovyov and Pavel Vinogradov . Call sign: Rodniki, so Rodnik-1 and Rodnik-2. During the first pass in orb. 2 (1838-1841 UTC) very weak signals on beacon- and telephony frequencies. During the pass in orb. 3 (2007-2011 UTC) very good reception on all frequencies. Solovyov could be heard in a conversation with TsUP. He reported a technical anomaly in the BO (life compartment): a hose (or: tube) was not connected to an air purification unit, which caused an increased amount of CO2 in the mini-atmosphere on board. He told TsUP that he had connected that hose immediately and that the system was functioning normally. Again good signals in the window in orb. 4 (2138-2147 UTC) during which Solovyev repeated his report about that hose.

    Mir:

    During the passes in the evening of 4.08.1997 the crew reported that they were working on the malfunctioning Elektron oxygen generator in Kvant-1. (The Elektron in Kvant-2 is not operational due to power shortages). During a long communication session via Altair-2 in the morning of 5.08.1997 the crew was still co-ordinating the repair work on the Elektron. After the departure of Progress-M35 for a 10 day lasting autonomous flight lithium perchlorate cartridges have to be used for the production of oxygen. This will be not very convenient during the period in which 5 men are on board (7-14.08.97).

    An eventual delay of the Soyuz-TM26 launch due to the problems with the Elektrons has not been taken into consideration.

    In MirNEWS.374 I gave an estimated time for the docking of Soyuz-TM26 on 7.08.97 as 1723 UTC. In that report I remarked that this time considerably deviated from the normal routine: dockings a few minutes after LOS of the first pass of both objects for our position. Inquiries in the Ballistic Section of the Keldysh institute of the R.A.N. learned that there had been a misprint in a Russian message about the estimated docking time. The estimated docking time is: 07.08.97 at 1703 UTC, so in accordance with the normal routine.

    The supply ship Progress-M35 has to free the docking port (+X-axis) for the arrival of the Soyuz-TM26 and will do this on 6.08.97 at 1144 UTC. The autonomous flight of Progress-M35 will last until 16.08.97. On that day Progress-M35 will dock (in the automatic regime with the system Kurs) at the same docking port after the redocking of Soyuz-TM26 to the forward (-X-axis) the day before. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 8 - Mir News 376: Soyuz-TM26. 

    This transport ship docked at the aft port of Mir on 7.08.1997 at 17.02.08 UTC. During the docking operation communications took place via Altair-2. The approach was in the automatic mode with the system Kurs. When Mir and Soyuz-TM26 came within my VHF-range Solovyov could be heard reporting distances, approach speeds and deviations in course. Everything went perfect until appr. 1700 UTC when a slight upward deviation forced Solovyov to take over manually. The 'Kurs' failure did not get much attention due to the euphoria after the 'successful' docking.

    Opening of the hatches:

    The hatches swung open during the pass in orb. 65507 at 1832 UTC. Normally this is a smooth and orderly procedure but this time there were some problems with the TV-link. Cheerfully both crews met each other. During the pass in orb. 65508, 2006-2013 UTC, TsUP and Solovyov discussed the conservation of the Soyuz-TM26 and some technical items. The session was concluded by the transfer of radiograms from Earth to Mir by Packet Radio.

    Communications during the 2d flight day of Soyuz-TM26:

    In all passes good reception on all frequencies. In a conversation with someone on Earth Vinogradov told that he somewhat suffered from space sickness during the first flight day and in the morning of the 2d one, but after eating somewhat substantial he recovered and was now feeling well.

    Progress-M35: This supply ship undocked from Mir on 6.08 at 11.46.45 UTC.

    Mir:

    Thus far Tsibliyev and Lazutkin did not succeed in repairing the Elektron oxygen generator in Kvant-1. There are some options to solve the problem: 1. With a spare part to be delivered by Atlantis in September, or 2. to try to find a way to deliver power to the Elektron in the now curtailed module Kvant-2. For the time being oxygen has to be generated by the heating of lithium perchlorate cartridges. Not so convenient with 5 men on board.

    Plans:

    (as far as known at deadline for this report) : Return of Tsibliyev and Lazutkin with their Soyuz-TM25 on 14.08.1997. (In my opinion a return of the relieved crew as soon as possible due to the oxygen problems would be a logical decision).

    The redocking of Soyuz-TM26 with on board Solovyov, Vinogradov and Foale from aft to forward docking port (P.Kh.O.) on 15.08. 1997.

    The return and docking in the automatic mode (Kurs) of Progress-M35 at the aft docking port on 16.08.1997. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 14 - Mir News 377: Soyuz-TM25. 

    This ship separated from on 14.08.97 at 08.55.58 UTC and flew away at 09.01.57 UTC.

    The return capsule (S.A.) of Soyuz-TM25 made a safe landing on 14.08.97 at 12.17.10 UTC at a distance of appr. 160 KM S.E. of Dzjeskazgan in Kazakhstan. The landing took place later than estimated and CNN did not bring the landing as 'live event'. For a long time TsUP could not give the exact spot where the S.A. came down. The radio traffic in which the farewell ceremony took place, and in which the relieved crew went on board Soyuz-TM25 and closed the hatches took place via the facilities of White Sands and Wallops in the U.S.A. and the tracking stations in the East of Russia.

    When Mir and Soyuz-TM25 entered daylight at abt. 1118 UTC communications with TsUP were established via Altair-2 in which Mir relayed traffic from and to Soyuz-TM25 via Altair-2 to TsUP. At abt. 1122 UTC Tsibliyev reported the beginning of the de-orbit burn. He reported continuously the results of the impulses in meters/sec and at 1126 UTC he said that the de-orbit burn had stopped. He went on reporting details of the descent process and at 1145 UTC he announced the separation of the BO (life compartment) and the instrument/motor module from the SA (descent module) in 3 minutes. This took place at 1148 UTC just before the 3 objects entered the dense layers of the atmosphere.

    The BO and Instrument/motor block burnt up and the SA came in the plasma wave. Radio contact ceased and contrary to previous return flights did not come back via Altair. The voices of the men on board Mir could be heard. Foale said that he had seen the Soyuz-TM25 disappearing below them. Altair-2 was switched off at 1201 UTC.

    Plans for tomorrow (15.08): Redocking of Soyuz-TM26 with on board the 3 crew members of Mir from the aft to the forward docking port. After undocking from Mir Soyuz-TM26 will hover and wait until Mir turned 180 dgs so that the forward (P.Kh.O.) port will be in front of Soyuz-TM26. During this operation lasting from abt. 1322-1410 UTC the crew will carry out an extensive photo- and video observation for damage assessment.

    Progress-M35: As far as known at deadline for this report Progress-M35 will redock at Mir's aft docking port on 17.08.97 at abt 1330 UTC. (So not as suggested in previous reports on 16.08.1997).

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 14 - Landing of Soyuz TM-25. 

    Following a mission that seemed to consist of an endless series of collisions, breakdowns, fires, and other emergencies, the EO-23 crew handed over the station to EO-24 and on August 14 entered Soyuz TM-25 landed in Kazakstan at 12:17 UTC, 170 km SE of Dzezkazgan. The Soyuz landing rockets failed to fire on touchdown, giving one of the roughest landings experienced by a returning Mir crew.

  • 1997 August 17 - Mir News 378: Progress-M35. 

    The redocking of this 'old' supply ship at the Mir complex did not take place on 17.08. During the first 3 passes of both objects it was obvious that Progress-M35 was continuing her autonomous flight. During the second pass the deputy head of mission control, Viktor Blagov, told the crew about changes in the work schedule for the next 2 days. The IVA would remain on schedule for 20.08.97.

    Reason postponement: The data for the approach of Progress-M35 today transmitted by TsUP to the Progress-M35 turned out to be wrong and Progress-M35's OBC shut itself off. At deadline for this report the docking of Progress-M35 at Mir was (still) planned for 18.08 at 1257 UTC.

    Soyuz-TM26: The redocking of this transport ship from the aft to the forward docking port took place on 15.08.97 between 13.29.20 and 14.13.04 UTC. At 1327 UTC, so just before separation, radio traffic from Soyuz-TM26 via Altair-2 could be heard. The safety clamps of the docking mechanism had been loosened and the program was proceeding according to plan. At 13.29.20 UTC Solovyov reported the separation and the fact that Soyuz-TM26 was slowly moving away from Mir. S. steered Soyuz-TM26 in the manual mode to be able to adjust the attitude of the ship in such a way that Vinogradov and Foale could make good images of the 'damage areas'.

    At 13.29.51 UTC Altair-2 transmitted an image of the whole complex seen by a camera of the ship. At 13.35.59 UTC S. reported the proceedings of the flight. He asked Foale whether he already was doing his photo- and video work and asked him for instructions to adjust the ship's attitude for the best images. Communications via Altair-2 ceased at 13.42.58 UTC, but a few minutes later S. could be heard via 121.750 mc (1401-1409 UTC). 4 minutes later S. accomplished a perfect docking at the forward (P.Kh.O. - transition section) port of the complex.

    Back on board Mir S. told TsUP that the images they had made were very good and certainly useful for analyses. In a conversation with Earth Foale told that they intended to transmit these images to TsUP on 18.08 and he was sure that TV stations all over the world would retransmit these. (The TV shots which already had been shown by TV stations came from short direct links with Russian tracking stations.)

    Elektron: Already on the day of the return of the relieved crew Vinogradov succeeded in restoring the Elektron oxygen generator in Kvant-1. It was very difficult to reach the spot where he had to clean Elektron. A white-brown jelly-like substance had stopped up a pipe inside Elektron and had to be cleaned. After purging this pipe he was able to restart Elektron and after 1 orbit Solovyov reported that Elektron was working normally. As far as could be derived from radio traffic Elektron still does thus far.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 19 - Mir News 379: Mir video transmissions. 

    In the morning of Monday 18.08 Mir transmitted to Earth video films and images made during the redocking of Soyuz-TM26 on 15.08. These transmissions took place during a Mir-Altair-2 window between 0542-0628 UTC. At 0601 UTC the crew stopped transmitting images and switched over to the co-ordination of IVA preparations with TsUP. During these activities the IVA was still scheduled for 20.08. This day Progress-M35 returned to the complex and docked at the aft docking port at 12.52.47 UTC. 10 Seconds later both objects disappeared behind the eastern horizon.

    Radio traffic during the beginning of the final phase of the docking operation went via Altair-2. Progress-M35 was at a distance of 800 M from Mir and the approach speed was 11.31 cm/sec. The crew of Mir observed the approaching supply-ship on a display of the LIV camera. A few minutes before the objects came in my range Altair-2 had been switched off and at 1246 UTC traffic went on via 143.625mc. S. reported distances and approach speeds. At 125045 UTC the distance was 12 M. At a distance of appr. 4 M. at 125156 UTC Kurs did not work. (Later on it turned out that Kurs had switched itself off at a distance of 20 M due to an irregularity in the attitude of Mir).

    After the docking of Progress-M35 I did not get time to relax for Geoff Perry told me that TsUP just had informed the press about a failure of the main OBC of Mir, the Ts.V.M.-1. Very often such failures happened before and it always causes a breakdown of the SUD (attitude control). The SUD is responsible for the good functioning of the gyrodynes and consequently these gyroscopes cry off. Commander Solovyov experienced a Ts.V.M.-1 failure in 1995 when he and Budarin made an autonomous flight with Soyuz-TM21 during the departure of Atlantis from Mir. S. immediately docked his ship, went aboard Mir and restored the Ts.V.M.-1.

    During all available passes in the evening Mir and TsUP discussed the problems. A specialist on Earth uttered the possibility that there was something wrong with the Ts.M.O. (central exchange module), an interface of the Ts.V.M.-1. He told the crew how to find that module and he gave them instructions for the repair. Foale told one of his countrymen in Moscow about his experiences during the final approach of Progress-M35. Through the viewer of his video camera he saw the Progress-M35 coming in very fast and he realised that something was wrong. He said: oh, no not again.. At that moment Progress-M35 slowed down and stopped and Solovyov took over manually.

    Foale emphasised that Progress-M35's computer had switched off Kurs due to divergence in the attitude of Mir. This was for Solovyov the signal to switch over to manual control. S. performed a perfect docking: in fact the Kurs system as well as the TORU remote control worked well. Situation in the evening of 19.08.97: The crew used the Soyuz-TM26 for the stabilisation of Mir's attitude and in the course of 19.08 the solar panels delivered twice as much energy as they did on 18.08. Meanwhile the Ts.V.M.-1 has been repaired and was ready for tests. At this point it was not known whether attitude control of the complex was provided by gyrodynes. .

    The crew resumed preparations for the IVA now planned for Friday 22.08.97 or Saturday 23.08.97. ECG's of the 'spacewalkers' have been transmitted to Earth and Solovyov as well as Vinogradov had already put on their spacesuits and checked the communication facilities and the electrical contacts of these suits.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 August 22 - EVA Mir EO-24-1.  Spacecraft: Mir.

    Connected Spektr power cables. Surveyed interior of depressurised Spektr module. Retrieved equipment and belongings from module.

  • 1997 August 25 - Mir News 380: Internal Spacewalk (IVA). 

    Internal Spacewalk (IVA) accomplished on 22.08.97 from 1114-1430 UTC. Some minor technical irregularities caused a delay of more than 2 hours. The crew worked according to a checklist (cyclogram). This checklist contained hundreds of items. The activities according to this checklist continued when the Mir was out of range of tracking stations or the geostationary Altair-2. This time Altair-2 was in use for phone conversations only. Altair-2 was active long before the IVA began, for instance during orbit 65734 from 0640-0732 UTC. The crew donned their spacesuits and Foale went on board Soyuz-TM26.

    According to plan the preparations for the IVA had to be concluded and the hatch to Spektr had to be opened during the window in orb. 65735, 0826-0910 UTC. A valve (KVD) between the P.Kh.O. and one of the modules (possibly module-T) could not be closed which caused a delay of about 1 hour.

    In orbit 65736 (0958-1043 UTC) all went well and at 1015 UTC the pressure in P.Kh.O. (serving as airlock for this IVA) was 50 mm. At that moment the pressure in the space suit of Vinogradov decreased due to a leak in his left glove. The crew immediately repressurised the P.Kh.O. They did this before the end of the window and Vinogradov could put on a spare glove. At 1114 UTC when the Mir was out of range the hatch to Spektr had been opened.

    Orbit 65737, 1135-1216 UTC.:

    IVA going on. All went well. Solovyov had joined Vinogradov inside the module. Vinogradov had already connected cables at the connectors of the new hatch and except for a single cable he did not met problems. During this window and the following one (orb. 65738/39, 1310-1400 UTC) V. and S. inspected the interior of Spektr and retrieved a lot of thus far not specified items from there. During these activities they consulted Foale. Vinogradov reported that he saw ventilators and pumps which were still working. He and S. did not find traces of exploded monitors or test-tubes. They did not succeed in finding places where the hull of Spektr had been penetrated. At last V. and S. left the Spektr to prepare the closure of the hatch. Foale , keeping a log book, reported that the hatch had been closed at 1430 UTC.

    After repressurising the P.Kh.O. in orb. 65740 (1448-1528 UTC), Foale joined his colleagues over there. In a short statement he expressed his admiration for the achievements of his crew mates and those on Earth who had been working on this operation. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 3 - Mir News 381: Power supply. 

    Vinogradov worked hard on the deployment of cables from the Spektr hatch to other modules and gradually he succeeded in restoring a part of the power supply for the modules Kvant-2 and Kristall. The 3 undamaged solar panels of Spektr delivered power, but rotation to achieve maximum solar illumination is not yet possible. Solovyov struggled along to keep Elektron in Kvant-1 operational and he also used power for the restoration of the Elektron in Kvant-2. On 25.08 Elektron in Kvant-1 shut itself off and the TGK (the solid fuel oxygen generator) did not work due to a defective firing pin. Before the outbreak of the usual press panic the cosmonauts had already repaired the TGK and Elektron in Kvant-1. The power supply is partly restored in Kvant-2 and Kristall: the lights are burning, the heating functions again and the drying process is going on.

    EVA preparations:

    Solovyov and Foale were convinced that they would get green light for the EVA on 6.09 and they started the preparations. Several times they donned their Orlan-M suits, checked all systems and took a stock of all the equipment needed for the EVA. Foale saw a film of his EVA training with Budarin in TsPK. He and S. also reviewed the so called 'cyclogram' of the EVA. The training of Foale during which Solovyov was instructor served also as a test to determine whether Foale will be able to do the EVA or not.

    Communications:

    The Altair-2 is regularly in use for communications between Mir and TsUP. They use this satellite for phone as well as for TV. On 1, 2 and 3.09 they showed images of their training, also with their space suits on, but also now and then video films of the interior and the outer surface of the complex. If on 4.09.1997 a positive decision will be taken the EVA will be made on 6.09.97. Opening of the hatch: 0055 UTC; planned duration 5 hrs 40 mins. Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 6 - EVA Mir EO-24-2.  Spacecraft: Mir.

    Inspected exterior of Spektr. Moved solar arrays.

  • 1997 September 6 - Mir News 382: Spacewalk.. 

    Spacewalk (EVA):

    The EVA began on 6.09 at 0107 UTC (hatch open) and ended at 0707 UTC (hatch closed). Everything went well. Directed by the old hand Solovyov (this was his 10th EVA!) Foale did all what he was supposed to do. His main job was the operation of the Strela , the crane to transport Solovyov to Spektr. Regularly instructed by Solovyov he did this in a perfect way. Vinogradov observed the 'spacewalkers' from inside Mir, helped them with advice and made images using video- and other camera's. After 0230 UTC the Russians used every 'window' of Altair-2, but mainly for phone only. Towards the end of the first window there was a short video transmission in which images made by Vinogradov could be monitored. The inspection of the outer surface of Spektr lasted longer than planned.

    Solovyov reported about the damages suffered by Spektr. One solar panel and some radiators were severely damaged. Support struts were broken or buckled. Solovyov did not find holes or punctures. The planned installation of a cap for the outlet valve for a Vozdukh CO2 scrubber in the Base Block has been put back until another EVA.

    During the EVA everybody was in a good mood. Although Solovyov had a difficult task to perform , even now and then his gasping could be heard, he was fully in control of the situation. Before entering the air-lock Foale had dismantled an American radiation dosimeter for retrieval.

    At abt. 0702 UTC both 'spacewalkers' entered the air-lock and at 0704 UTC Foale got orders to close the hatch. Initially the hatch could not be closed, but after using some extra effort Foale could report at 0707 UTC that he had succeeded. Solovyov confirmed this after seeing an indicator showing the sign 'hatch closed'.

    This time for the Russians MOLODTSY and for Foale: WELL DONE.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 10 - Mir News 383: Progress-M35. 

    This old supply-ship has been keeping watch at the aft (Kvant-1) docking port as of 18.08, the day of the redocking. Due to the well-known priorities the crew has not paid any attention to this ship until 8.09.97. One of the first tasks of the this day was the opening of the hatch and the inspection of Progress-M35's interior. The main function of the Progress-M35 was the protection of the docking mechanism of Kvant-1 against the sun. The freighter has still room in which garbage and other no longer needed material can be stowed. During the first pass for our position in orb. 65998 (0522 UTC) preparations for the opening of the hatch were going on. The crew got permission to open the hatch after the air seal checks. During the next pass in orb. 65999 ( the Russians consider this orbit to be number 66000) the hatch had already been opened but Solovyov had set this ajar for the smell which came out of the Progress-M35 was far from a 'kurort smell'. The crew however had to cease all activities with the Progress-M35 due to other concerns.

    Main Computer failure:

    In the pass in orb. 65999 TsUP wants to discuss the air seal check with Vinogradov. V. interrupts TsUP with the statement that a few minutes ago (exactly 0700 UTC) the Ts.V.M.-1 had shut itself down. After this report followed the usual chain reaction: the SUD (system for movements- or attitude control) stopped and Foale reported that this was also the case with the SUD in Module-D (Kvant-2). Systems like SRV-U (regeneration of water from urine) and Elektron had to be switched off. TsUP gave orders to burn 3 lithium perchlorate cartridges for oxygen generation. (Solovyov stated repeatedly that the delivery of a new supply of those cartridges during mission STS-86 is badly needed.) Foale reported that the angle of the solar panels to the sun was unfavourable, but that the complex though inclining a little bit on one side, was stable. In passing TsUP stated that they have a jubilee: the 66000th orbit of Mir's Base Block. This statement did not evoke joyful reactions or congratulations.

    In spite of the complicated situation on board there was some excitement: the 'scapegoats of the space era' ,Tsibliyev and Lazutkin, visited TsUP and had a short conversation with their colleagues in space. Foale, the crewman with a great sense of humour, told Tsibliyev that his 'darling' the SUD, again chucked the thing. After a short conversation with these 2 poor guys on earth about the fact that they would depart for a vacation, the crew set back to work.

    About the computer:

    The crew restarted the computer, but failed to find the cause of the failure. So they switched the computer off. A specialist told Vinogradov that there must be a spare Ts.M.O. on board which eventually could be used to replace the present Ts.M.O. (Central Module for Data exchange). The failure of the Ts.V.M.-1 during the redocking operation of the Progress-M35 had probably been caused by a defective Ts.M.O. In the course of the day it was obvious that the crew had everything under control and that the repair of the computer was successfully proceeding. During the night Solovyov was on duty to keep his eye on the situation and to assist TsUP during the reloading of the repaired computer. In the morning of 9.09 Solovyov was still on duty during the first pass over here in orbit 66013, 0427 UTC.

    Depending on the state of the SEP (Power supply system) they would power up the rest of the gyrodyne's this day. During the next pass Vinogradov was on duty and Solovyov tried to get some rest in his sleeping bag. Already 6 gyrodyne's were spinning, the Elektron had been switched on, lights were burning and ventilators were buzzing again. Vinogradov reported about the problems he had met while powering up the computer. He had met the same problems like Lazutkin a few weeks ago.

    Stabilisation:

    At the beginning of the next day (10.09) it was obvious that the situation had been stabilising gradually. All available gyrodyne's were functioning and the crew could eventually restart experiments. The main activity consisted of the reanimation of the Module Priroda. The interior of this module will be dried with hot air. To blow this hot air into the module air-hoses are used.

    Next spacewalk (EVA):

    After the arrival of Progress-M36 in the beginning of October.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 16 - Mir News 384: Priroda. 

    Drying out of this module lasted longer than expected. In the evening of 11.09 Vinogradov collected 8 litres of condense water.

    Kristall:

    This module is dry. This is not the case with the SO (docking compartment) attached at Kristall. The crew supposed that they have to dry out this SO in the same way as they do with Priroda.

    On 14.09 TsUP asks Vinogradov whether the crew already used condensation for drinking water. Analyses of water samples delivered on earth on 14.08 should justify the potable use of water from condensation. Vinogradov said that they did not thus far, but that they have used this water for the refilling of the Elektron.

    On 14.09 at 1028 UTC the crew got orders to switch off the Ts.V.M.-1 (Main OBC). Telemetry indicated that 2 of the 3 channels (possibly interfaces) of that computer produced incorrect data. Due to the better charged accumulators this time the usual 'chain-reaction' was not as abrupt as during Ts.V.M.-1 failures in the past. Nevertheless the SUD, the attitude control, switched itself off and the gyrodynes slowed down and stopped. The Elektron, which consumes 1 kW was switched off. The complex came in the so called 'free drift'.

    When on 15.09 the station passed over here for the 3d time in orb. 66107 (0509 UTC) the cosmonauts had switched on the Ts.V.M.-1 as well as the SUD. This was only for a short period. Later on both systems were 'off'. The cosmonauts got permission to dismantle the computer and to replace some parts and/or accessories. At TsUP considerations were going on about the replacement of this computer by a reserve which has been in stock for a long time if the repairs might fail. At last the decision was taken to have the whole computer replaced and so the crew did. In the evening the cosmonauts rebooted the 'new' computer. In the night from 15 to 16.09 Solovyov was on duty while experts at TsUP loaded data in the computer. As soon as the computer was operational the attitude of the complex could be stabilised.

    On 16.09 at 02.15.03 UTC the orientation was restored in such a manner that recharging of the accumulators could begin. Radio traffic revealed that the situation was normalising. A number of systems, among which the Elektron, remained off. For oxygen production the cosmonauts continued to use 'disks' (lithium perchlorate cartridges). The pressure of Mir's atmosphere was 618 mm mercury.

    More computer news:

    Progress-M36 has to deliver a brand-new computer in October this year.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 22 - Mir News 385: MAIN COMPUTER FAILURE. 

    On 22.09 at 0123 UTC the crew was waked up by the alarm signal: Check the SUD (attitude control). When they did they saw that the Ts.V.M.-1, the main computer had switched itself off. Solovyov reported this to TsUP during the pass over here in orbit 66214, 0130-0140 UTC. The first system to be switched was again the oxygen generator Elektron.

    During the pass in orb. 66215, 0305-0316 UTC, S. reported that initially the attitude of the complex was not so good. The complex is flying the so called free drift. The supply from the solar panels decreased to a level of 200 Amperes.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 September 26 - STS-86.  Spacecraft: Atlantis. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Atlantis was launched on a mission to the Russian Mir space station. The TI rendevous terminal initiation burn was carried out at 17:32 GMT on September 27, and Atlantis docked with the SO (Docking Module) on the Mir complex at 19:58 GMT. The crew exchange was completed on September 28, with David Wolf replacing Michael Foale on the Mir crew. On October 1 cosmonaut Titov and astronaut Parazynski conducted a spacewalk from the Shuttle payload bay while Atlantis was docked to Mir. They retrieved four MEEP (Mir Environmental Effects Payload ) exposure packages from Mir's SO module and installed the Spektr solar array cap. The MEEP experiments had been attached to the Docking Module by astronauts Linda Godwin and Rich Clifford during Shuttle mission STS-76 in March 1996. In addition to retrieving the MEEP, Parazynski and Titov were to continue an evaluation of the Simplified Aid For EVA Rescue (SAFER), a small jet-backpack designed for use as a type of life jacket during station assembly.

    Atlantis undocked from Mir at 17:28 GMT on October 3 and conducted a flyaround focused on the damaged Spektr Module to determine the location of the puncture in its hull. The Mir crew pumped air into the Spektr Module using a pressure regulator valve, and the Shuttle crew observed evidence that, as expected, the leak seemed to be located at the base of the damaged solar panel. Final separation of Atlantis from Mir took place around 20:28 GMT. After two landing attempts were waved off on October 5 due to heavy cloud cover, the crew fired the engines to deorbit at 20:47 GMT on October 6 and landed at Kennedy Space Center at 21:55.

  • 1997 September 26 - Spacehab Double Module.  Spacecraft: Spacehab. Launch Site: Cape Canaveral. Launch Vehicle: Shuttle.

    Remained attached to OV-104

  • 1997 September 29 - Mir News 386: Computer failure. 

    Compared to computer failures in the past the crew was able to restore the situation very quickly. In the night from 22 to 23.09 the crew successfully rebooted the same computer which they had replaced last week. The computer which failed on 22.09 had been stored for a long period in a cold and wet module.

    The following day the crew restarted a number of gyrodynes. Another failure they had to cope with was a malfunctioning ventilator of the Vozdukh, the CO2 filter. The replacement of this ventilator was easy, but the crew lost much time in finding a spare. The crew changed their sleep schedule to prepare for the arrival of Atlantis and for the period in which Atlantis will be attached to Mir. To be sure that the computer will remain operational the crew used an air duct for cooling. The gyrodynes functioned normally on 24.09 and so did the Vozdukh. During a direct TV-session in the early morning of 25.09 Foale commented images from the interior of the Base Block and explained the problems with the computer. He also showed some video-recordings of his EVA on 6.09.

    Launch of Atlantis for mission STS-86:

    On 26.09 at 0234 UTC Atlantis was launched while Mir flew over Europa and communicated with TsUP. The crew was listening to a direct report of the launch. No reaction could be monitored for Mir disappeared over the horizon.

    Atlantis, communications:

    Exactly 19 minutes after the launch (0253-0300 UTC) Atlantis was in our range and communicated with Houston via a tracking station in Spain. Wetherbee reported a minor failure which he should ignore. So he did with some other minor problems. He assured Houston to keep an eye on those matters.

    Docking Atlantis:

    In the course of 27.09 one of the channels of the computer behaved in a strange way. This lasted only a few milliseconds. A long time before the rendezvous Atlantis and Mir were in range of each other enabling both crews were to communicate via direct VHF-channels. Regretfully this all took place out of our range. At abt. 1900 UTC Atlantis reached a point at 200 Metes below Mir. From there by the use of the R-bar (or radial vector) approach she gently drifted to Mir with only a few little corrections with steering rockets by Wetherbee. After altering his approach due to a minor deviation of the attitude of the Mir-complex he flawlessly docked Atlantis at Mir. The Russians reported this success with the words 'kasaniye and zakhvat' (touch and capture). After a few minutes followed the hard mate and the airtight checks. The equalisation gave some problems: Foale felt pain is his ears and in Spacehab an alarm indicated that the equalisation was proceeding too quickly.

    For me it was a pleasure to hear Titov again from Mir. Almost 9 years ago he left Mir after being in space for 366 days. (He then returned to earth together with Jean Loup Chretien, who had been in Mir for almost a month.)

    Relief:

    On the first full day of the Atlantis/Mir link-up Wolf replaced Foale as a member of the Mir crew, when Wolf's seat liner for his seat in the Soyuz-TM26 had been installed in this ' ferry- and rescue vehicle'. Wolf will use the Module-D as his working- and living quarters. He will sleep in the airlock of that module.

    Radio traffic Mir:

    During the Atlantis/Mir link-up Mir will use the communications facilities of the Shuttle as well as the normal Mir frequencies. The Shuttle is also equipped with the 130.165 mc, the so called VHF-1. On board of the Shuttle this channel is AB-2. In the night from 28 to 29.09 Mir communicated with TsUP Moscow on 143.625 mc. During this traffic TsUP reported that the Shuttle was flying in 'free drift'. This took place in the framework of an attitude control experiment. During the next pass for our position at abt. 2200 UTC the Shuttle was in control of the attitude again.

    Spacewalk (EVA):

    This EVA will be made by Parazynski and Titov and is scheduled for 1.10 between 1844-2334 UTC (date and timeline not yet fully confirmed). The astronauts will retrieve a container with the MEEP experiment and 'park' a cap which might be necessary for the repair of Spektr's hull. In fact this will be an American EVA and the astronauts will enter open space through the airlock of the Shuttle. During the windows in which Atlantis/Mir is in range it might be worthwhile to monitor Shuttle's EVA frequency 279.000 mc (mode AM-Wide).

    Installation of the new computer:

    Possibly this computer will be installed during the Atlantis/Mir link-up. A final decision still has to be taken. If so this will be done after the EVA. If circumstances demand this the link-up of Atlantis and Mir can be extended by 24 hours.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 October 1 - EVA STS-86-1.  Spacecraft: Mir.

    Retrieved MEEP materials exposure experiment from outside of Mir.

  • 1997 October 5 - Progress M-36.  Spacecraft: Progress M. Mass: 7,195 kg (15,862 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz.

    Unmanned resupply vessel to Mir. Docked with Mir on 8 Oct 1997 17:07:09 GMT. Undocked on 17 Dec 1997 06:01:53 GMT. Destroyed in reentry on 19 Dec 1997 13:20:01 GMT. Total free-flight time 5.39 days. Total docked time 69.54 days.

  • 1997 October 6 - Mir News 387: Communications Mir during mission STS86. 

    The communications to and from the Mir during the link-up period of Atlantis and Mir demonstrated what we can expect when of the International Space station the Russian and American segments will be operational. For matters regarding the whole complex the American side will take care for the communications and traffic between the Russian segment and TsUP-M will only concern Russian matters (experiments, maintenance, advice, etc.) The lion's share of the communications went via Atlantis. During windows in which the Mir was able to communicate via Russian tracking facilities they only handled Russian matters. The communications between Mir and Atlantis took place via an intercom system. Sometimes Atlantis also took care of the Packet Radio traffic for Mir. During the link-up Mir seldom used the Altair-2 facility. Images of the approach of Atlantis and the EVA of Parazynski and Titov made from inside Mir were directly transmitted to earth via Russian tracking stations on UHF frequencies. Sometimes the comments on those images went via the VHF channel. On 28.09 Altair-2 was in use for the relay of video-recordings.

    Progress-M36:

    This freighter blasted off from Baykonur on 5.10.1997 at 15.08.57 UTC. All went well. The Progress-M36 will deliver the normal cargo: water, food, fuel, experiments and a spare computer. Among the repair material is a special glue ('germetik') to be used during the repair of the Spektr. Progress-M36 is expected to dock at Mir's aft docking port (Kvant-1 +X axis) on 7.10 at 1642 UTC.

    Transmissions Progress-M36:

    On 5.10 during the 3d orbit (1944-1946 UTC) Telemetry was heard in the 165 and 166 mc bands. During the 4th orbit (2114-2119 UTC) the signals in the 165 and 166 mc were very strong. The transmitter on 922.755mc was active during that pass. TCA was at 21.15.54 UTC

    Progress-M35:

    This old freighter is no longer needed and will separate from Mir on 6.10 at 1124 UTC for a short autonomous flight and decay in the atmosphere over a designated area in the Pacific East of New Zealand at 1424 UTC.

    Mini-sputnik:

    A small copy of Sputnik-1 will also be delivered by Progress-M36. During the next EVA of Solovyov and Vinogradov on 16.10.1997 this Sputnik will be 'launched' manually. This satellite will send 'bleeps' on a frequency in the 2 Meter amateur band to recall the launch of the first artificial earth satellite on 4.10.1957.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 October 6 - Landing of STS-86. 

    STS-86 landed at 21:55 GMT with the crew of Wetherbee, Bloomfield, Titov Vladimir, Parazynski, Chretien, Lawrence and Foale aboard.

  • 1997 October 7 - Mir News 388: Progress-M35. 

    The undocking of this freighter failed on 6.10 at 1124 UTC. Cause was a human error: the crew had forgotten to remove a clamp from the docking mechanism (the Russian word is 'styazhka', a clamp or spanner to tighten the docking). The Russians decided to postpone the undocking until 7.10. On 7.10.1997 at 12.03.47 UTC Progress-M35 separated from Mir and after a short period in which Progress-M35 hovered at a distance of 10 Meters Progress-M35 moved away for a short autonomous flight. The decay in the atmosphere over a designated area in the Pacific East of New Zealand will take place at 1734 UTC.

    Progress-M36:

    The docking of this freighter at Mir has been put back until 8.10.1997 at 1713 UTC.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 October 9 - Mir News 389: Progress-M36. 

    On 8.10 at 17.07.40 UTC, so 7 minutes earlier than planned, this freighter docked at Mir's aft docking port (+X axis). Approach and docking took place in the automatic mode by the system Kurs. Solovyov was ready to take over manually with TORU in case of a Kurs failure. During the operation the crew stayed in the Base Block. The opening of the hatches was put back until 9.10 at 0830 UTC.

    Spacewalks (EVA's):

    For a while an external EVA was scheduled for 16.10, but this plan was cancelled. The first EVA (in fact an IVA) will take place inside the module Spektr and will be made on 20.10 at 0900 UTC. Depending on the results of that IVA the Russians will determine date and working method for the following EVA. During that EVA the cosmonauts will 'jettison' the miniature Sputnik, recently delivered by Progress-M36.

    Radio-amateur traffic:

    The Packet radio on 145.985 mc is very active and now and then this transmitter is used for phone. David Wolf, also using the call R0Mir, already has a liking for these activities.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 October 15 - Mir News 390: Progress-M36. 

    The opening of the hatches took place on 9.10 at abt 0830 UTC. Thus far the crew did not spend much time for the unloading of the ship. Among the normal cargo Progress-M36 delivered the spare SUD (attitude control) computer, the mini-sputnik-1 and the German/Russian satellite Inspector. On 12.10 during a long TV-session via Altair-2 with relatives the crew showed the little Sputnik.

    Mir-routine:

    The crew replaced some accumulators in the Base Block and the Module-D (Kvant-2) and rearranged other batteries to ensure a better charging. Now and then the crew has to collect condensation water. Vinogradov reported that the module Priroda is dry.

    The next spacewalk (EVA, so this time an IVA) will be made inside the module Spektr. This is the 3d one for this Mir-crew (the 3d for Solovyov) the 2d for Vinogradov. The IVA is on schedule for 20.10 from 0855 UTC and will last about 5 hrs 30 mins. The preparations for this IVA began after the arrival of Progress-M36 and intensified from 13.10.97. The crew will have to replace an electronic unit in the Spektr. This unit has to control the servomotors to aim the solar panels. The unit in the Spektr did not survive the vacuum in that module and will be replaced by the same device still installed in the module Kristall. On 13 and 14.10 the cosmonauts worked on the spacesuits (this time again the Orlan-DMA). They connected tanks, devices, a.s.o. and checked the airtightness. On 14.10 the crew continued the preparations for the work to be done. On 15.10 they underwent medical tests.

    The 4th EVA Mir-crew:

    This external spacewalk is tentatively scheduled for 3.11.97. During this EVA they will have to remove the old solar panel on the module E (Kvant-1). The new Russian solar panel which is still stored at the outer surface of the SO (docking compartment) will be installed during an EVA in the future.

    Minor technical problems:

    Now and then minor technical problems emerge: On 10.10 a minor repair of the Elektron and the BKV (a.c.) and in the evening TsUP derives from Telemetry that the pressure in a KOB (heating loop) increased. On 12.10 they had to economise electrical energy and to switch off some systems. On 14.10 a ventilator of the Vozdukh CO-2 scrubber failed and had to be switched off. During the next orbit the Vozdukh worked well.

    David Wolf:

    David is very busy with his experiments. He even sometimes had no time for lunch. Like his predecessor Foale he also handles the Packet Radio traffic on the service channel. In a conversation with relatives (possibly his parents and grandmother) he said that all was well, but that he was yearning for a pizza and a beer. Now and then David can be heard during radio-amateur traffic on 145.985 mc.

    Mini-sputnik-1:

    This little satellite (3 KG) will be jettisoned during the first EVA, so possibly on 3.11.97. The transmissions can be heard on 145.800 mc. The output will be 0.2 Watt. The antenna polarisation is circular, but as there is no attitude control the received signal may have clockwise or counter clockwise polarisation. The modulation will be FM and the audio tone about. 1.3 kc varying with the temperature. The endurance of the power supply batteries will be about 30 days.

    Chris v.d. Berg, NL-9165/A-UK3202.

  • 1997 October 20 - EVA Mir EO-24-3.  Spacecraft: Mir.

    Installed new hatch to reconnect Spektr solar array cable with Mir power bus.

  • 1997 October 22 - Mir News 391: Rehearsal Internal spacewalk (IVA) on 17.10.1997. 

    This rehearsal lasted some hours. David Wolf stayed in the descent module of the Soyuz-TM26 ship from where he now and then communicated with TsUP or his working crew mates. Solovyov and Vinogradov tried to train for the IVA as realistically as possible. The original plan to replace the steering interface for the solar panels from the Kristall to the Spektr module had been abandoned: installing this device with clumsy spacesuit gloves is a 'mission impossible'. So the only way to insert the Kristall interface in the circuitry for the servomotors of the solar panels on Spektr was to deploy cables from the connection for these motors to the interface in Kristall. During the IVA Vinogradov has to connect 3 cables between the servomotors and the inside of the vacuum plate.

    Progress-M36:

    During the IVA the docking device of this freighter had to be depressurised. On Saturday, 18.10 the crew could not open a valve for this depress. Solovyov compared this with an equal experience he had during his short stay in Mir in June 1988, when Vladimir Titov was the commander. Probably the failure was caused by a failing switch. The crew resolved the problem on 19.10.

    IVA on 20.10:

    Opening of the hatch 45 minutes later than planned at 0940 UTC. The delay was caused by the fact that it lasted longer to put on the Orlan-DMA spacesuits and a valve to one of the modules which failed to close. When the hatch was opened Mir was still out of range of the Altair-2 Comm. Sat . Vinograd