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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.
- 1986 February 19 - Mir. Spacecraft: Mir . Mass: 20,100 kg (44,300 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K.
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 11A511U2.
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 April 23 - Progress 26. Spacecraft: Progress. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 28 - EVA Mir EO-1-1. Spacecraft: Mir.
Installed truss.
- 1986 May 31 - EVA Mir EO-1-2. Spacecraft: Mir.
Tested truss structure.
- 1987 March 31 - Kvant 1. Spacecraft: Kvant. Mass: 20,000 kg (44,000 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K.
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 21 - Progress 29. Spacecraft: Progress. Mass: 7,100 kg (15,600 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 11A511U2.
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 July 22 - Soyuz TM-3. Spacecraft: Soyuz TM. Mass: 7,100 kg (15,600 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 August 3 - Progress 31. Spacecraft: Progress. Mass: 7,212 kg (15,899 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 11A511U2.
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 December 21 - Soyuz TM-4. Spacecraft: Soyuz TM. Mass: 7,070 kg (15,580 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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.
- 1988 May 13 - Progress 36. Spacecraft: Progress. Mass: 7,077 kg (15,602 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 June 7 - Soyuz TM-5. Spacecraft: Soyuz TM. Mass: 7,000 kg (15,400 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 July 18 - Progress 37. Spacecraft: Progress. Mass: 7,065 kg (15,575 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 11A511U2.
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 11A511U2.
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 November 26 - Soyuz TM-7. Spacecraft: Soyuz TM. Mass: 7,000 kg (15,400 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 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 11A511U2.
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 March 16 - Progress 41. Spacecraft: Progress. Mass: 6,995 kg (15,421 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 September 5 - Soyuz TM-8. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 8K82K.
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 11A511U2.
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 February 11 - Soyuz TM-9. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 May 31 - Kristall. Spacecraft: Kristall. Mass: 19,640 kg (43,290 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K.
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 August 1 - Soyuz TM-10. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 September 27 - Progress M-5. Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 December 2 - Soyuz TM-11. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 March 19 - Progress M-7. Spacecraft: Progress M. Mass: 7,307 kg (16,109 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 May 18 - Soyuz TM-12. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 August 20 - Progress M-9. Spacecraft: Progress M. Mass: 7,311 kg (16,117 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 11A511U2.
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.
- 1992 February 20 - EVA Mir EO-10-1. Spacecraft: Mir.
Dismantled equipment.
- 1992 June 30 - Progress M-13. Spacecraft: Progress M. Mass: 7,320 kg (16,130 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 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 11A511U2.
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.
- 1993 May 22 - Progress M-18. Spacecraft: Progress M. Mass: 7,348 kg (16,199 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 July 1 - Soyuz TM-17. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 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...more.
- 1993 October 11 - Progress M-20. Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U.
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.
- 1994 January 8 - Soyuz TM-18. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 May 22 - Progress M-23. Spacecraft: Progress M. Mass: 7,117 kg (15,690 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U.
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 August 25 - Progress M-24. Spacecraft: Progress M. Mass: 7,250 kg (15,980 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U.
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 October 3 - Soyuz TM-20. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 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 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.
- 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 March 14 - Soyuz TM-21. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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 May 12 - EVA Mir EO-18-1. Spacecraft: Mir.
Retracted solar array.
- 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 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 11A511U.
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 September 3 - Soyuz TM-22. Spacecraft: Soyuz TM. Mass: 7,150 kg (15,760 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U2.
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.
- 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 May 5 - Progress M-31. Spacecraft: Progress M. Mass: 7,140 kg (15,740 lb). Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U.
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.
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