Encyclopedia Astronautica
Mir EO-5



qmirmmu.jpg
Soyuz TM-8
Test of SPK Manned Manoeuvring Unit
Credit: RKK Energia
isouztm8.jpg
Mir EO-5
Credit: www.spacefacts.de - www.spacefacts.de
Crew: Serebrov, Viktorenko. Attached the new Kvant-2 module to the station; conducted five spacewalks; tested the Soviet UMK manned maneuvering unit. Backup crew: Balandin, Solovyov.

The Mir Expedition EO-5 docked with Mir on 8 September. The Mir orbital station team consisted of A S Viktorenko, commander of the spacecraft, and A A Serebrov, on-board engineer. The crew attached the new Kvant-2 module to the station and conducted five spacewalks in installation activities and test of the Soviet YMK manned maneuvering unit. Total mission cost was given as 80 million rubles, with an expected return of 25 million rubles net profit.

Narrative (adapted from D S F Portree's Mir Hardware Heritage, NASA RP-1357, 1995)

Soyuz TM-8 arrived at Mir after five months during which the station was uninhabited. The Kvant-2 and Kristall modules were now ready for launch, and the station began its second period of expansion. On September 29 the cosmonauts installed equipment in the docking system in preparation for the arrival of Kvant 2, the first of Mir's 20-ton add-on modules. Solar storm warnings. On September 30 a powerful flare burst out on the Sun. Initial predictions indicated that the cosmonauts could receive many times the maximum permissible level of radiation. In the event, the cosmonauts received only about as much radiation as they would normally receive in two weeks of flight.

It was announced on October 10 that problems with a batch of computer chips pushed back the launch of Mir's second add-on module by at least 40 days from the planned October 16 launch date. The major focus of Viktorenko and Serebrov's mission was to receive, check out, and activate the module, so their schedule underwent heavy revision.

Kvant 2 was launched on November 26. Soon after launch the TsUP discovered that the right solar array had not deployed properly, allowing it to flop freely. By rolling Kvant 2 and rotating the array simultaneously, the TsUP was able to fully extend and lock the array. On December 2 Kvant 2 closed to within 20 m of the Mir front port before its Kurs control system terminated the approach. It had sensed that the module was moving too fast. Problems also developed on Mir: the Argon 16B control computer shut down the attitude control gyrodynes in Kvant after detecting an error. Viktorenko and Serebrov assumed manual control of Mir for the second attempt, which was successful. The Lyappa manipulator arm on Kvant 2 then inserted itself into a fixture on the multiport docking node and pivoted the module into place at the top lateral port. The transfer required about 1 hr

On 12 December the crew flew Soyuz TM-8 from the aft port of Mir and docked to the forward port now cleared of the Kvant-2 module. Progress-M 2 arrived at Mir and remained docked to the aft port from December 22, 1989-February 9, 1990

The new guidance control computer for Mir, the Salyut 5B system delivered by Kvant 2, needed star sensors more capable than those in place on Kvant. On January 8, in the first of the EVAs postponed from Principal Expedition 4, Viktorenko and Serebrov opened one of the three free docking node hatches, transferred the twin 80-kg sensor packages outside, and installed them on Kvant. Start of the 2-hr, 56-min EVA was delayed 1 hour by a depressurisation problem in Soyuz TM-8—when the cosmonauts lowered pressure in the docking node, an improperly set valve released air from the spacecraft as well.

On January 11 the cosmonauts became the last to use a docking node hatch for an EVA. They removed for return to Earth the Enchantillons space exposure experiment rack set up by Chretien during his December 1988 EVA, removed and discarded the ERA platform installed by Chretien and Volkov, and made modifications to the docking node in preparation for the arrival of the next large module, Kristall.

Cosmos 2054, the third Altair/SR geosynchronous satellite took up position at 344° E in mid-January. It was launched on December 27, 1989. Combined with Cosmos 1897, it permitted Mir to maintain contact with the TsUP in Moscow about 70% of the time.

On January 26 Viktorenko and Serebrov donned new Orlan-DMA spacesuits. These were improved versions of the Orlan suits they had worn on their first two EVAs. They then entered and depressurized the special EVA airlock compartment at the outboard end of Kvant 2. The EVA airlock hatch is wider than the docking hatches (1 m vs 0.8 m) to permit passage of the YMK, the Soviet MMU equivalent, which is stored in Kvant 2. The central instrument-science compartment of Kvant 2 can also be sealed and depressurised, expanding the size of the airlock and providing a backup. The cosmonauts attached a mooring post to the outside of the airlock compartment and removed a Kurs antenna so it could not interfere with future EVAs. EVA duration was 3 hr, 2 min.

The Soviet "flying armchair" manoeuvring unit weighed 218 kg and had been delivered to the station aboard Kvant-2. Serebrov donned the unit on February 1 and moved up to 33 m from the station. In case the YMK malfunctioned, during the test he was bound by a tether attached to a winch on the mooring post installed on the previous EVA. The EVA lasted 4 hr, 59 min.

On February 5 Viktorenko flew the YMK to a distance of 45 m. He carried the Spin-6000 device, which measured radiation from Mir induced by cosmic ray bombardment. EVA duration was 3 hr, 45 min.

On February 13 the EO-6 relief crew of Balandin and Solovyov arrived at the station aboard Soyuz TM-9. Soon after they arrived in orbit, Balandin and Solovyov noted that three of eight thermal insulation blankets on their spacecraft's descent module had come loose at their lower (heat shield) ends and were waving about as the spacecraft manoeuvred in space. It was thought they could block optical navigation sensors, and that the damaged insulation might cause the spacecraft to overheat or cool down so much that condensation would form on its optical equipment. The possibility existed that an electrical short might occur if condensation developed on equipment. Docking with Mir occurred as normal. The cosmonauts and TsUP worked out procedures by which the TsUP monitored Soyuz TM-9's temperature and manoeuvred Mir to move it in and out of sunlight as needed to maintain proper temperature. In the meantime, cosmonauts worked in the hydrolab training facility in Zvezdny Gorodok, outside Moscow, to develop EVA repair procedures. Consideration was also given to sending a rescue Soyuz-TM carrying a single cosmonaut to pick up the cosmonauts and return them to Earth.

The problem was considered manageable and the Soyuz TM-8 crew had an uneventful return to earth after a productive mission.

AKA: Vityaz (Knight ); Soyuz TM-8.
First Launch: 1989.09.05.
Last Launch: 1990.02.19.
Duration: 166.29 days.

More... - Chronology...


Associated People
  • Serebrov Serebrov, Aleksandr Aleksandrovich (1944-) Russian engineer cosmonaut. Flew on Salyut 7 EP-2, Soyuz T-8, Mir EO-5, Mir EO-14. Ten spacewalks. 372 cumulative days in space. Civilian Engineer, Energia NPO. Civilian Engineer, Energia NPO. More...
  • Viktorenko Viktorenko, Aleksandr Stepanovich (1947-) Russian pilot cosmonaut. Flew on Mir EP-1, Mir EO-5, Mir EO-11, Mir EO-17. 489 cumulative days in space. Call sign: Vityaz (Knight). More...
  • Solovyov Solovyov, Anatoliy Yakovlevich (1948-) Russian test pilot cosmonaut. Flew on Mir EP-2, Mir EO-6, Mir EO-12, Mir EO-19, Mir EO-24. 651 cumulative days in space. More...
  • Balandin Balandin, Aleksandr Nikolayevich (1953-) Russian engineer cosmonaut. Civilian Engineer, Energia NPO. Flew on Mir EO-6. Left cosmonaut corps for medical reasons and returned to NPO Energia until departing in 1994. Then President of Lendint-Association until 2000. More...

See also
Associated Programs
  • Mir 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. More...

Mir EO-5 Chronology


1989 August 23 - . 03:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 T15000-037.
  • Progress M-1 - . Payload: Progress M s/n 201. Mass: 7,270 kg (16,020 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-5. Spacecraft: Progress M. Duration: 100.34 days. Completed Operations Date: 1989-12-01 11:21:28 . Decay Date: 1989-12-01 11:21:28 . USAF Sat Cat: 20191 . COSPAR: 1989-066A. Apogee: 217 km (134 mi). Perigee: 187 km (116 mi). Inclination: 51.6000 deg. Period: 88.50 min. 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 - . 21:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Soyuz TM-8 - . Call Sign: Vityaz (Knight ). Crew: Serebrov; Viktorenko. Backup Crew: Balandin; Solovyov. Payload: Soyuz TM 11F732 s/n 58. Mass: 7,150 kg (15,760 lb). Nation: USSR. Related Persons: Serebrov; Viktorenko; Balandin; Solovyov. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EO-5. Spacecraft: Soyuz TM. Duration: 166.29 days. Decay Date: 1990-02-19 . USAF Sat Cat: 20218 . COSPAR: 1989-071A. Apogee: 392 km (243 mi). Perigee: 390 km (240 mi). Inclination: 51.6000 deg. Period: 92.40 min. 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 - . 13:01 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 354-01.
  • Kvant 2 - . Payload: 77KSD s/n 17101. Mass: 19,565 kg (43,133 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Kvant-2. Duration: 1,615.45 days. Decay Date: 2001-03-23 . USAF Sat Cat: 20335 . COSPAR: 1989-093A. Apogee: 397 km (246 mi). Perigee: 388 km (241 mi). Inclination: 51.6000 deg. Period: 92.40 min. 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 - . 03:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 T15000-039?.
  • Progress M-2 - . Payload: Progress M s/n 202. Mass: 7,300 kg (16,000 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-5. Spacecraft: Progress M. Duration: 51.18 days. Completed Operations Date: 1990-02-09 07:56:10 . Decay Date: 1990-02-09 07:56:10 . USAF Sat Cat: 20373 . COSPAR: 1989-099A. Apogee: 392 km (243 mi). Perigee: 390 km (240 mi). Inclination: 51.6000 deg. Period: 92.40 min. 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 - . 20:23 GMT - .
1990 January 11 - . 18:01 GMT - .
  • EVA Mir EO-5-2 - . Crew: Viktorenko; Serebrov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.12 days. Nation: USSR. Related Persons: Viktorenko; Serebrov. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Mir. Summary: Retrieved and installed material samples.

1990 January 26 - . 12:09 GMT - .
  • EVA Mir EO-5-3 - . Crew: Viktorenko; Serebrov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.13 days. Nation: USSR. Related Persons: Viktorenko; Serebrov. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Mir. Summary: Tested spacesuit. Examined exterior of Kvant 2..

1990 February 1 - . 08:15 GMT - .
  • EVA Mir EO-5-4 - . Crew: Viktorenko; Serebrov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.21 days. Nation: USSR. Related Persons: Viktorenko; Serebrov. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Mir. Summary: Serebrov tested SPK manoeuvring unit..

1990 February 5 - . 06:08 GMT - .
  • EVA Mir EO-5-5 - . Crew: Viktorenko; Serebrov. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.16 days. Nation: USSR. Related Persons: Viktorenko; Serebrov. Program: Mir. Class: Manned. Type: Manned space station. Flight: Mir EO-5. Spacecraft: Mir. Summary: Viktorenko tested SPK manoeuvring unit..

1990 February 11 - . 06:16 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Soyuz TM-9 - . Call Sign: Rodnik (Spring - water spring). Crew: Balandin; Solovyov. Backup Crew: Manakov; Strekalov. Payload: Soyuz TM 11F732 s/n 60. Mass: 7,150 kg (15,760 lb). Nation: USSR. Related Persons: Balandin; Solovyov; Manakov; Strekalov. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EO-5; Mir EO-6. Spacecraft: Soyuz TM. Duration: 179.05 days. Decay Date: 1990-08-09 . USAF Sat Cat: 20494 . COSPAR: 1990-014A. Apogee: 387 km (240 mi). Perigee: 373 km (231 mi). Inclination: 51.6000 deg. Period: 92.20 min. 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 - .
Home - Browse - Contact
© / Conditions for Use