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Salyut 7
Part of Almaz
Kosmos 1267/Salyut 7
Kosmos 1267 / Salyut 7. This detailed painting was the first revelation in the West of the configuration of the TKS spacecraft.
Russian manned space station, launched 1982-04-19. Salyut 7 was the back-up article for Salyut 6 and very similar in equipment and capabilities. However the crews were able to conduct significant military experiments due to the greatly increased volume and payload of the TKS modules diverted from the cancelled Almaz program that docked with the station.
AKA: 11F715;17KS s/n 126;DOS-6. Status: Operational 1982. First Launch: 1982-04-19. Last Launch: 1982-04-19. Number: 1 . Thrust: 3.92 kN (881 lbf). Gross mass: 19,824 kg (43,704 lb). Unfuelled mass: 18,624 kg (41,058 lb). Specific impulse: 305 s. Height: 14.40 m (47.20 ft). Span: 17.00 m (55.00 ft).
Cancellation of the Almaz military station and delays in the Mir project led to the decision was taken in the late 1970's to fly the back-up to DOS-5 / Salyut 6. This was launched as Salyut 7 in 1982. The opportunity was taken to continue to fly 'guest cosmonauts' from friendly countries on short visits to the stations, although emphasis was placed on military experiments.
Salyut 7 was aloft for four years and two months, during which time it was visited by 10 crews constituting 6 main expeditions and 4 secondary flights (including French and Indian cosmonauts). A total of 22 cosmonauts visited the station, five of them twice and one three times. From two to six crew were aboard at any one time. 11 Soyuz T and 15 Progress spacecraft made a total of 25 dockings and 3 redockings. Mission durations of 211 and then 237 days were achieved, during which 13 EVA's were conducted during 861 total days of piloted flight. Due to various technical problems, Salyut 7 was much less productive a space station than Salyut 6.
On 19-22 August 1986 the station was moved to a 474 km x 492 km orbit, which was expected to take a very long time to decay. Retrieval at a future date by a Buran shuttle was planned. However much greater than expected solar activity resulted in it returning to earth much more rapidly than expected.
Due to various technical problems, Salyut 7 was much less productive a space station than Salyut 6. Equipment aboard Salyut 7 included a Unitary Propulsion/RCS Systems, Kurs Rendezvous/Docking System, 24 hr hot water, and a food refrigerator. Experimental Equipment included the Kristal materials processing furnace; EFO-7 star electrophotometer; an Improved Oasis plant growth unit; an Aelita cardiovascular diagnostic unit; a French echography ultrasonic medical system; and a Korund semiconductor materials furnace. Military experiments conducted with equipment delivered aboard TKS modules included observations of ground aerosols; ABM intercept detection and tracking equipment; naval exercises; and laser pointing/tracking hardware tests.
The manned ferry to the station was the Soyuz T, derived from the still-born Soyuz 7K-S military version of Soyuz which began development in 1968. Station resupply was by Progress, an unmanned logistics modification of the Soyuz that replaced the crew re-entry vehicle with propellant tanks. Large TKS modules from the cancelled Almaz program docked with Salyut 7 for major military experiments. From 17 July 1984 Soyuz could be launched with 200 kg additional mass thanks to use of Tsiklin propellant in the Soyuz-U2 booster.
RCS Coarse No x Thrust: 14 X 98 N. RCS Fine No x Thrust: 18 x 10 N. Electric System: 2.00 average kW.
More at: Salyut 7.
Subtopics
Family:
Soviet Space Stations,
Space station,
Space station orbit.
People:
Grechko,
Volk,
Chretien,
Savinykh,
Ivanchenkov,
Strekalov,
Lyakhov,
Kizim,
Malyshev,
Berezovoi,
Lebedev,
Polyakov,
Dzhanibekov,
Aleksandrov,
Malhotra,
Serebrov,
Romanenko,
Popov,
Baudry,
Solovyov, Vladimir,
Titov, Vladimir,
Viktorenko,
Volkov, Aleksandr,
Savitskaya,
Sharma,
Atkov,
Ivanova,
Saley,
Vasyutin,
Pronina.
Country:
Russia.
Engines:
KRD-79.
Spacecraft:
Progress,
Soyuz T,
Iskra,
Salyut 7,
Astrozond.
Flights:
Salyut 7/TKS-2,
Soyuz T-5,
Soyuz T-6,
Soyuz T-7,
Salyut 7/TKS-3,
Soyuz T-8,
Soyuz T-9,
Soyuz T-10-1,
Soyuz T-10,
Soyuz T-11,
Soyuz T-12,
Soyuz T-13A,
Soyuz T-13 EO-4-a,
Soyuz T-13 EO-4-b,
Soyuz T-14 EO-4-c,
Soyuz T-14 Salyut 7 EP-5,
Soyuz T-15A,
Soyuz T-15B,
Soyuz T-15C.
Launch Vehicles:
Proton,
Proton-K,
Soyuz-U,
Soyuz-U2.
Propellants:
N2O4/UDMH.
Launch Sites:
Baikonur,
Baikonur LC200/40.
Agency:
Korolev bureau,
MOM,
UNKS.
Bibliography:
2,
21,
274,
299,
32,
33,
367,
51,
6,
66,
67,
89,
6851.
Photo Gallery
| Salyut 7 in Assembly Salyut 7 in Assembly Hall Credit: RKK Energia |
| Salyut 7 frozen. The frozen interior of Salyut 7 that greeted the crew of the Soyuz T-15 repair mission. Credit: RKK Energia |
| Salyut 7 Credit: © Mark Wade |
| Salyut 6 Credit: Manufacturer Image |
1982 April 19 - .
19:45 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
- Salyut 7 - .
Payload: Zarya s/n 125-2. Mass: 18,900 kg (41,600 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned space station. Spacecraft Bus: Almaz.
Spacecraft: Salyut 7.
Duration: 3,215.34 days. Decay Date: 1991-02-07 . USAF Sat Cat: 13138 . COSPAR: 1982-033A. Apogee: 284 km (176 mi). Perigee: 279 km (173 mi). Inclination: 51.60 deg. Period: 90.20 min.
Second Soviet replenishable long-duration 'civilian' space station. Objectives: Continuation of scientific research on board manned space complexes in the interests of science and the Soviet national economy; testing of advanced systems and apparatus for orbital stations. Continuation of the scientific research in progress on board manned space complexes in the interests of science and the national economy; testing of advanced systems and apparatus for orbital stations. Although of the same design as Salyut 6, technical breakdowns throughout its life made Salyut 7 a much less productive station. Replaced finally by Mir. Two different TKS resupply craft, originally designed for the Almaz military station, docked with Salyut 7 to provide a larger complex. With the cancellation of Almaz, a large proportion of the experiments carried out on board had military objectives. As of January 1990 out of fuel, unable to manoeuvre, uncontrolled re-entry expected in three to four years. Re-entered in 1991 with 70 kg fuel remaining over Argentina. Controllers attempted to control impact point (set for Atlantic Ocean) by setting Salyut 7/Kosmos 1686 assembly into a tumble. This however failed and Salyut 7 re-entered February 7, 1991 04:00 GMT. Many fragments fell on the town of Capitan Bermudez, 25 km from Rosario and 400 km from Buenos Aires, Argentina. At 1 am local time the sky was lit up with hundreds of incandescent meteors travelling from Southwest to Northeast. At dawn the inhabitants discovered numerous metal fragments, which seemed to have fallen in distinct groups at various locations in the city. Luckily no one was hurt in the metallic shower. Additional Details: here....
- Iskra 2 - .
Payload: RK-02. Mass: 28 kg (61 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Communications.
Type: Amateur radio communications satellite. Spacecraft: Iskra.
Decay Date: 1982-07-09 . USAF Sat Cat: 13176 . COSPAR: 1982-033C. Apogee: 345 km (214 mi). Perigee: 336 km (208 mi). Inclination: 51.60 deg. Period: 91.40 min. Deployed from Salyut 7 5/17/82. Launched from Salyut 7. Experiments in amateur radio communications. Launched into orbit from aboard the Salyut-7 orbital scientific station. .
1982 May 13 - .
09:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-5 - .
Call Sign: Elbrus (Elbrus - tallest mountain in Europe). Crew: Berezovoi,
Lebedev.
Backup Crew: Strekalov,
Titov, Vladimir.
Payload: Soyuz T s/n 11L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-5.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 106.21 days. Decay Date: 1982-08-27 . USAF Sat Cat: 13173 . COSPAR: 1982-042A. Apogee: 231 km (143 mi). Perigee: 190 km (110 mi). Inclination: 51.60 deg. Period: 88.70 min. Carried Anatoli Berezovoi, Valentin Lebedev to Salyut 7 to conduct scientific research and experiments; returned crew of Soyuz T-7 to Earth..
1982 May 23 - .
05:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1982 June 24 - .
16:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-6 - .
Call Sign: Pamir (Pamirs ). Crew: Chretien,
Dzhanibekov,
Ivanchenkov.
Backup Crew: Baudry,
Kizim,
Solovyov, Vladimir.
Payload: Soyuz T s/n 9L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-5,
Soyuz T-6.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 7.91 days. Decay Date: 1982-07-02 . USAF Sat Cat: 13292 . COSPAR: 1982-063A. Apogee: 233 km (144 mi). Perigee: 189 km (117 mi). Inclination: 51.70 deg. Period: 88.70 min.
Manned three crew. Docked with Salyut 7. Transported to the Salyut-7 orbital station the Soviet-French international crew, comprising V A Dzhanibekov (USSR), A S Ivanchenkov (USSR) and Jean-Loup Chretien (France) to conduct scientific research and experiments.
1982 July 2 - .
1982 July 10 - .
09:57 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 14 - .
Payload: Progress s/n 117. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-5.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 33.65 days. Completed Operations Date: 1982-08-13 11:29:16 . Decay Date: 1982-08-13 11:29:16 . USAF Sat Cat: 13361 . COSPAR: 1982-070A. Apogee: 325 km (201 mi). Perigee: 301 km (187 mi). Inclination: 51.60 deg. Period: 90.70 min. Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 12 Jul 1982 11:41:00 GMT. Undocked on 10 Aug 1982 22:11:00 GMT. Destroyed in reentry on 13 Aug 1982 01:29:00 GMT. Total free-flight time 4.21 days. Total docked time 29.44 days..
1982 July 30 - .
02:39 GMT - .
1982 August 19 - .
17:11 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-7 - .
Call Sign: Dnepr (Dnieper ). Crew: Popov,
Savitskaya,
Serebrov.
Backup Crew: Pronina,
Romanenko,
Savinykh.
Payload: Soyuz T s/n 12L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-5,
Soyuz T-7.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 113.08 days. Decay Date: 1982-12-10 . USAF Sat Cat: 13425 . COSPAR: 1982-080A. Apogee: 299 km (185 mi). Perigee: 289 km (179 mi). Inclination: 51.60 deg. Period: 90.30 min. Docked with Salyut 7. Carried Svetlana Savitskaya, Leonid Popov, Alexander Serebrov to Salyut 7 to conduct scientific and technical research and experiments..
1982 August 27 - .
Late 1982 - .
1982 September 18 - .
04:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 15 - .
Payload: Progress s/n 112. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-5.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 28.51 days. Completed Operations Date: 1982-10-16 17:08:06 . Decay Date: 1982-10-16 17:08:06 . USAF Sat Cat: 13558 . COSPAR: 1982-094A. Apogee: 241 km (149 mi). Perigee: 188 km (116 mi). Inclination: 51.70 deg. Period: 88.80 min. Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 20 Sep 1982 06:12:00 GMT. Undocked on 14 Oct 1982 13:46:00 GMT. Destroyed in reentry on 16 Oct 1982 17:08:00 GMT. Total free-flight time 4.19 days. Total docked time 24.32 days..
- Astrozond - .
Payload: Astrozond. Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Flight: Soyuz T-5.
Spacecraft: Astrozond.
Decay Date: 1982-10-28 . USAF Sat Cat: 13596 . COSPAR: 1982-033AC. Apogee: 364 km (226 mi). Perigee: 307 km (190 mi). Inclination: 51.60 deg. Period: 91.24 min.
1982 October 31 - .
11:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 16 - .
Payload: Progress s/n 115. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-5.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 44.25 days. Completed Operations Date: 1982-12-14 17:16:24 . Decay Date: 1982-12-14 17:16:24 . USAF Sat Cat: 13638 . COSPAR: 1982-107A. Apogee: 246 km (152 mi). Perigee: 186 km (115 mi). Inclination: 51.60 deg. Period: 88.80 min. Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 2 Nov 1982 13:22:00 GMT. Undocked on 13 Dec 1982 15:32:00 GMT. Destroyed in reentry on 14 Dec 1982 17:17:00 GMT. Total free-flight time 3.16 days. Total docked time 41.09 days..
1982 November 18 - .
11:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/40.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
- Iskra 3 - .
Payload: RK-03. Mass: 28 kg (61 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Communications.
Type: Amateur radio communications satellite. Flight: Soyuz T-5.
Spacecraft: Iskra.
Decay Date: 1982-12-16 . USAF Sat Cat: 13663 . COSPAR: 1982-033AD. Apogee: 356 km (221 mi). Perigee: 349 km (216 mi). Inclination: 51.60 deg. Period: 91.60 min. Launched from Salyut 7 airlock. Conduct of experiments in the field of amateur radiocommunications. .
1982 December 10 - .
During 1983 - .
1983 April 20 - .
13:10 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-8 - .
Call Sign: Okean (Ocean ). Crew: Serebrov,
Strekalov,
Titov, Vladimir.
Backup Crew: Aleksandrov,
Lyakhov,
Savinykh.
Payload: Soyuz T s/n 13L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-8.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 2.01 days. Decay Date: 1983-04-22 . USAF Sat Cat: 14014 . COSPAR: 1983-035A. Apogee: 213 km (132 mi). Perigee: 196 km (121 mi). Inclination: 51.60 deg. Period: 88.60 min. Manned three crew. Unsuccessful mission. Failed to rendezvous with Salyut 7. Recovered April 22, 1983 13:29 GMT. Landed 113 km SE Arkalyk..
1983 April 22 - .
1983 June 27 - .
09:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-9 - .
Call Sign: Proton (Proton ). Crew: Aleksandrov,
Lyakhov.
Backup Crew: Strekalov,
Titov, Vladimir.
Payload: Soyuz T s/n 14L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-9.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 149.45 days. Decay Date: 1983-11-23 . USAF Sat Cat: 14152 . COSPAR: 1983-062A. Apogee: 228 km (141 mi). Perigee: 197 km (122 mi). Inclination: 51.60 deg. Period: 88.80 min. Manned two crew. Docked with Salyut 7. Transported to the Salyut-7 orbital station a crew consisting of V A Lyakhov, commander of the spacecraft, and A P Aleksandrov, flight engineer, to conduct scientific and technical research and experiments..
1983 August 17 - .
12:08 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 17 - .
Payload: Progress s/n 119. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-9.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 31.48 days. Completed Operations Date: 1983-09-17 23:42:37 . Decay Date: 1983-09-17 23:42:37 . USAF Sat Cat: 14283 . COSPAR: 1983-085A. Apogee: 242 km (150 mi). Perigee: 189 km (117 mi). Inclination: 51.60 deg. Period: 88.80 min. Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 19 Aug 1983 13:47:00 GMT. Undocked on 17 Sep 1983 11:44:00 GMT. Destroyed in reentry on 17 Sep 1983 23:43:00 GMT. Total free-flight time 2.57 days. Total docked time 28.91 days..
1983 September 26 - .
19:37 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
FAILURE: Launch vehicle blew up on pad..
Failed Stage: 0.
- Soyuz T-10-1 - .
Call Sign: Okean (Ocean). Crew: Strekalov,
Titov, Vladimir.
Backup Crew: Kizim,
Solovyov, Vladimir.
Payload: Soyuz 7K-ST s/n 16L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: UNKS.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-10-1,
Soyuz T-9.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 0.0001 days. Decay Date: 1983-09-27 . Apogee: 2.00 km (1.20 mi). Aborted September 27, 1983 19:38 GMT. Unsuccessful mission. Launch vehicle blew up on pad at Tyuratam; crew saved by abort system..
1983 October 20 - .
09:59 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1983 November 1 - .
04:47 GMT - .
1983 November 3 - .
03:47 GMT - .
1983 November 23 - .
1984 February 8 - .
12:07 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1984 February 21 - .
06:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1984 April 3 - .
13:08 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-11 - .
Call Sign: Yupiter (Jupiter ). Crew: Malyshev,
Sharma,
Strekalov.
Backup Crew: Berezovoi,
Grechko,
Malhotra.
Payload: Soyuz T s/n 17L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-10,
Soyuz T-11.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 181.91 days. Decay Date: 1984-10-02 . USAF Sat Cat: 14872 . COSPAR: 1984-032A. Apogee: 224 km (139 mi). Perigee: 195 km (121 mi). Inclination: 51.60 deg. Period: 88.70 min.
Manned three crew. Docked with Salyut 7.Transported a Soviet-Indian international crew comprising ship's commander Y V Malyshev, flight engineer G M Strekalov (USSR) and cosmonaut-researcher R Sharma (India) to the SALYUT-7 orbital station to conduct scientific and technical studies and experiments.
1984 April 11 - .
1984 April 15 - .
08:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
1984 April 23 - .
04:31 GMT - .
1984 April 26 - .
02:40 GMT - .
1984 April 29 - .
01:35 GMT - .
1984 May 4 - .
23:15 GMT - .
1984 May 7 - .
22:47 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1984 May 18 - .
17:52 GMT - .
1984 May 28 - .
14:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1984 July 17 - .
17:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Soyuz T-12 - .
Call Sign: Pamir (Pamir mountains). Crew: Dzhanibekov,
Savitskaya,
Volk.
Backup Crew: Ivanova,
Savinykh,
Vasyutin.
Payload: Soyuz T s/n 18L. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-10,
Soyuz T-12.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 11.80 days. Decay Date: 1984-07-29 . USAF Sat Cat: 15119 . COSPAR: 1984-073A. Apogee: 218 km (135 mi). Perigee: 192 km (119 mi). Inclination: 51.60 deg. Period: 88.60 min. Docked with Salyut 7. Transported a crew comprising ship's commander V A Dzhanibekov, flight engineer S E Savitskaya and cosmonaut-research I P Volk to the Salyut-7 orbital station to conduct scientific and technical studies and experiments..
1984 July 25 - .
14:55 GMT - .
1984 July 29 - .
1984 August 8 - .
08:46 GMT - .
1984 August 14 - .
06:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1984 October 2 - .
1985 March - .
1985 June 6 - .
06:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
1985 June 21 - .
00:39 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1985 July 19 - .
13:05 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1669 - .
Payload: Progress s/n 126. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz T-13 EO-4-a,
Soyuz T-13 EO-4-b.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 41.51 days. Completed Operations Date: 1985-08-30 01:19:52 . Decay Date: 1985-08-30 01:19:52 . USAF Sat Cat: 15918 . COSPAR: 1985-062A. Apogee: 247 km (153 mi). Perigee: 187 km (116 mi). Inclination: 51.60 deg. Period: 88.80 min.
Progress vehicle, given Cosmos designation instead of Progress because control lost early in mission but regained later. Resupplied Salyut 7. On departure briefly undocked and redocked to verify reliability of docking system. Transported of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 21 Jul 1985 15:05:00 GMT. Undocked on 28 Aug 1985 21:50:00 GMT. Destroyed in reentry on 30 Aug 1985 01:20:00 GMT. Total free-flight time 3.23 days. Total docked time 38.28 days.
1985 August 2 - .
07:15 GMT - .
1985 September 17 - .
12:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U2.
- Soyuz T-14 - .
Call Sign: Cheget (Tcheget - mountain in the Caucasus). Crew: Grechko,
Vasyutin,
Volkov, Aleksandr.
Backup Crew: Saley,
Strekalov,
Viktorenko.
Payload: Soyuz T s/n 20L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 7.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-13 EO-4-a,
Soyuz T-13 EO-4-b,
Soyuz T-14 EO-4-c,
Soyuz T-14 Salyut 7 EP-5.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 64.91 days. Decay Date: 1985-11-21 . USAF Sat Cat: 16051 . COSPAR: 1985-081A. Apogee: 223 km (138 mi). Perigee: 196 km (121 mi). Inclination: 51.60 deg. Period: 88.70 min.
Docked with Salyut 7. Transported a crew comprising ship's commander V V Vasyutin, flight engineer G M Grechko and cosmonaut-researcher A A Volkov to the Salyut-7 orbital station to conduct scientific and technical studies and experiments. Grechko returned in Soyuz T-13 on 25 September 1985 - emergency return.
1985 September 26 - .
1985 November 21 - .
1986 Early - .
1986 June - .
1986 September - .
- Soyuz T-15C (cancelled) - .
Crew: Dobrokvashina,
Ivanova,
Savitskaya.
Backup Crew: Aleksandrov,
Solovyov,
Viktorenko.
Mass: 7,150 kg (15,760 lb). Nation: Russia.
Program: Salyut 7.
Flight: Soyuz T-15C.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Cancelled all-female flight to be launched on International Woman's Day, to have docked with Mir or Salyut 7. Breakdown of Salyut 7, exhaustion of stock of Soyuz T spacecraft, and official resistance led to cancellation of the mission. Officially cancelled due to birth of Savitskaya's baby. No female cosmonauts would be in training again until a decade later.
1991 February 6 - .
- Salyut-7 Burnup In Earth's Atmosphere (Soviet Union Space Station) - .
Nation: Russia.
Spacecraft Bus: Almaz.
Spacecraft: Salyut 7.
1991 February 7 - .
- Salyut 7 re-enters - .
Nation: Russia.
Program: Salyut 7.
Spacecraft Bus: Almaz.
Spacecraft: Salyut 7.
Salyut 7 had been put into a high storage orbit in June 1986, which was supposed to allow it to remain in orbit for ten years before decaying. But much greater than expected solar activity caused the orbit to decay rapidly. By the end of 1990 the station was no longer controllable, and on 7 February 1991 the station came down over South America.
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