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Salyut 6
Part of Almaz
Salyut 6
The Salyut 6 station as displayed in Moscow, November 1981. At the aft end a Progress resupply craft is docked. At the forward docking station is a Soyuz spacecraft, representing Soyuz 34 according to the lettering on the side. Unusually, the Soyuz Ferry (7K-T) spacecraft is shown with solar panels, which was thought never to be the case by Western observers.
Credit: © Mark Wade
Russian manned space station, launched 1977-09-29. The Salyut 6 space station was the most successful of the DOS series prior to Mir. It was aloft for four years and ten months, completing 27,785 orbits of the earth.
AKA: 11F715;17KS s/n 125;DOS-5. Status: Operational 1977. First Launch: 1977-09-29. Last Launch: 1977-09-29. Number: 1 . Payload: 1,500 kg (3,300 lb). Thrust: 5.88 kN (1,322 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).
Mishin was authorized in December 1973 to build an improved design DOS-5 version of the Salyut station using Almaz facilities. Mishin's bureau borrowed the two docking port configuration of Chelomei's Almaz OPS-2 This station's second docking port would allow rotation of crews and resupply/refueling using unmanned Progress spacecraft.
DOS-5 flew as Salyut 6 in 1977. The dual docking ports allowed near-continuous occupation of the station through crew rotation. The opportunity presented by the need to replace the Soyuz ferry spacecraft at ninety-day intervals was taken to fly 'guest cosmonauts' from friendly countries on short visits to the stations.The additional docking port also allowed resupply of the station using the Progress, an unmanned logistics vehicle. The Progress replaced the crew re-entry vehicle of the Soyuz with propellant tanks to replenish the station. The orbital module was stuffed with food, water, and equipment supplies.
Five main expeditions and 11 short duration expeditions visited the station, of which nine had international crews. A total of 676 days of piloted operations were conducted by 27 cosmonauts with steadily increasing flight duration: 18, 75, 96, 140, and 185 days. 35 automatic dockings were conducted with the station by 20 Soyuz, 12 Progress, and 1 TKS spacecraft.
Autopilot: Digital. Propulsion/RCS Systems: Unitary. Main propulsion 2 x 300 kgf, stabilization and orientation motors 32 x 24 kgf. Telemetry: High Rate. Rendezvous/Docking: Kurs. Equipment: - MKF-6 multispectral camera system - KT-140 high resolution topographical camera system (200,000 sq. km. per film frame) KRT-10 10 m diameter radio telescope - Splav alloying/materials processing furnace - Kristal containerless processor for semiconductor materials - BST-1M 1.5 m diameter cryogenic submillimeter/ ultraviolet/infrared telescope Refraktion and Zarya spectrometers for sun/moon views through earth's limb - Ispartitel experiment for coating of plates with materials - Yelena gamma ray telescope - Oasis plant growth unit - Polinom cardiovascular monitoring system.
Habitable Volume: 90.00 m3. RCS Coarse No x Thrust: 14 X 98 N. RCS Fine No x Thrust: 18 x 10 N. Electric System: 2.00 average kW.
Subtopics
Family:
Soviet Space Stations,
Space station,
Space station orbit.
People:
Gubarev,
Grechko,
Rukavishnikov,
Makarov,
Khrunov,
Bykovsky,
Gorbatko,
Kubasov,
Aksyonov,
Jaehn,
Jankowski,
Ryumin,
Koellner,
Savinykh,
Ivanov, Georgi,
Ivanchenkov,
Andreyev,
Strekalov,
Lyakhov,
Kizim,
Malyshev,
Hermaszewski,
Zudov,
Tamayo Mendez,
Kovalyonok,
Lebedev,
Polyakov,
Dediu,
Dzhanibekov,
Klimuk,
Pelczak,
Romanenko,
Popov,
Tuan,
Gurragcha,
Remek,
Ganzorig,
Liem,
Farkas,
Magyari,
Lopez Falcon,
Aleksandrov, Aleksandr,
Prunariu.
Country:
Russia.
Engines:
KRD-79.
Spacecraft:
Soyuz 7K-T,
Soyuz 7K-T/A9,
Soyuz 7K-S,
Salyut 6,
Progress,
Soyuz T,
KRT-10.
Flights:
Soyuz 25,
Soyuz 26,
Soyuz 27,
Soyuz 28,
Soyuz 29,
Soyuz 30,
Soyuz 31,
Soyuz 32,
Soyuz 33,
Soyuz 35,
Soyuz 36,
Soyuz T-2,
Soyuz 37,
Soyuz 38,
Soyuz T-3A,
Soyuz T-3,
Soyuz T-4,
Soyuz 39,
Soyuz 40.
Launch Vehicles:
Proton,
Proton-K,
Soyuz-U.
Propellants:
N2O4/UDMH.
Launch Sites:
Baikonur,
Baikonur LC81/24.
Agency:
Korolev bureau,
MOM.
Bibliography:
2,
21,
274,
32,
33,
51,
6,
66,
67,
89,
6850,
13051.
Photo Gallery
| Salyut 6 KRT-10 Salyut 6 KRT-10 deployment Credit: RKK Energia |
| Salyut 6 Engines Close-up of the engines of Salyut 6 as displayed in Moscow in 1981. Credit: © Mark Wade |
| Salyut 6 in Assembly Salyut 6 in Assembly Hall Credit: RKK Energia |
| Salyut 6 model Salyut 6 model showing cosmonaut on treadmill and bulk of solar camera on the right Credit: © Mark Wade |
| Salyut 6 In Space Credit: RKK Energia |
| Salyut 6 Cutaway The Salyut 6 space station was the first evolved design with two docking ports. Credit: RKK Energia |
| Salyut 6 Salyut 6 as displayed in Moscow in 1981. Credit: © Mark Wade |
| Salyut 6 Poster |
| Salyut 6 Credit: Manufacturer Image |
1975 September 29 - .
04:15 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 772 - .
Payload: Soyuz 7K-S s/n 2L. Mass: 6,750 kg (14,880 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-S.
Duration: 3.99 days. Decay Date: 1975-10-02 . USAF Sat Cat: 8338 . COSPAR: 1975-093A. Apogee: 245 km (152 mi). Perigee: 154 km (95 mi). Inclination: 51.80 deg. Period: 88.40 min.
Unmanned military Soyuz 7K-S test flight. Recovered October 3, 1975 4:10 GMT. Unsuccessful mission. Transmitted only on 166 MHz frequency, at none of the other usual Soyuz wavelengths.
Maneuver Summary:
193 km X 270 km orbit to 195 km X 300 km orbit. Delta V: 8 m/s
196 km X 300 km orbit to 196 km X 328 km orbit. Delta V: 8 m/s
Total Delta V: 16 m/s
1976 November 29 - .
16:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 869 - .
Payload: Soyuz 7K-S s/n 3L. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-S.
Duration: 17.77 days. Decay Date: 1976-12-17 . USAF Sat Cat: 9564 . COSPAR: 1976-114A. Apogee: 289 km (179 mi). Perigee: 209 km (129 mi). Inclination: 51.70 deg. Period: 89.40 min.
Unmanned military Soyuz 7K-S test flight. Recovered December 17, 1976 10:31 GMT. Transmitted only on 20.008 MHz and 166 MHz frequencies, at none of the other usual Soyuz wavelengths.
Maneuver Summary:
196 km X 290 km orbit to 187 km X 335 km orbit. Delta V: 15 m/s
187 km X 335 km orbit to 259 km X 335 km orbit. Delta V: 21 m/s
259 km X 335 km orbit to 260 km X 345 km orbit. Delta V: 2 m/s
260 km X 345 km orbit to 265 km X 368 km orbit. Delta V: 7 m/s
265 km X 368 km orbit to 267 km X 391 km orbit. Delta V: 6 m/s
267 km X 391 km orbit to 300 km X 310 km orbit. Delta V: 32 m/s
Total Delta V: 83 m/s
1977 September 29 - .
06:50 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC81/24.
LV Family:
Proton.
Launch Vehicle:
Proton-K.
- Salyut 6 - .
Payload: Zarya s/n 125 s/n 5L. Mass: 19,824 kg (43,704 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned space station. Spacecraft Bus: Almaz.
Spacecraft: Salyut 6.
Duration: 1,763.71 days. Decay Date: 1982-07-29 . USAF Sat Cat: 10382 . COSPAR: 1977-097A. Apogee: 237 km (147 mi). Perigee: 188 km (116 mi). Inclination: 51.60 deg. Period: 88.70 min.
Conduct of scientific and technical research and experiments; further testing of station design, on-board system and equipment. Soyuz 25 docking unsuccessful. EVA 20 Dec 1977 to examine forward docking port (no damage). EVA 29 July 1978 to retrieve externally mounted experiments (micrometeorites, biopolymers, radiation plates, materials tests). Soyuz 33 failure to dock due to propulsion failure April 1979. Soyuz 34 launched unmanned to provide replacement vehicle June 1979. EVA August 15 to dislodge 10 m diameter KRT-10 radio telescope from aft docking collar. Repair mission Soyuz T-3 December 1980 (temperature control hydraulics). Repair mission Soyuz T-4 March 1981 (stuck solar array). Salyut ejected a module on May 31 (perhaps retained Soyuz Orbital Module). Kosmos 1267 docks 19 June 1981. Commanded to reentry using Kosmos 1267 propulsion system over Pacific July 29 1982. Additional Details: here....
1977 October 9 - .
02:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 25 - .
Call Sign: Foton (Photon). Crew: Kovalyonok,
Ryumin.
Backup Crew: Ivanchenkov,
Romanenko.
Payload: Soyuz 7K-T s/n 42. Mass: 6,860 kg (15,120 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 25.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 2.03 days. Decay Date: 1977-10-11 . USAF Sat Cat: 10401 . COSPAR: 1977-099A. Apogee: 240 km (140 mi). Perigee: 194 km (120 mi). Inclination: 51.60 deg. Period: 88.80 min. Manned two crew. Unsuccessful mission. Failed to dock with Salyut 6..
1977 October 11 - .
1977 December 10 - .
01:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 26 - .
Call Sign: Taimyr (Taimyr - Russian peninsula). Crew: Grechko,
Romanenko.
Backup Crew: Ivanchenkov,
Kovalyonok.
Payload: Soyuz 7K-T s/n 43. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 26.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 37.42 days. Decay Date: 1978-01-16 . USAF Sat Cat: 10506 . COSPAR: 1977-113A. Apogee: 235 km (146 mi). Perigee: 205 km (127 mi). Inclination: 51.60 deg. Period: 88.80 min. Manned two crew. Docked with Salyut 6. Carried Yuri Romanenko, Georgi Grechko to Salyut 6; returned crew of Soyuz 27 to Earth. Conduct of joint experiments with the Salyut-6 scientific station..
1977 December 19 - .
21:36 GMT - .
1978 January 10 - .
12:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 27 - .
Call Sign: Pamir (Pamir mountains). Crew: Dzhanibekov,
Makarov.
Backup Crew: Ivanchenkov,
Kovalyonok.
Payload: Soyuz 7K-T s/n 44. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 26,
Soyuz 27.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 64.95 days. Decay Date: 1978-03-16 . USAF Sat Cat: 10560 . COSPAR: 1978-003A. Apogee: 237 km (147 mi). Perigee: 190 km (110 mi). Inclination: 51.70 deg. Period: 88.70 min. Manned two crew. Carried Oleg Makarov, Vladimir Dzhanibekov to Salyut 6; returned crew of Soyuz 26 to Earth. Docked with Salyut 6..
1978 January 16 - .
1978 January 20 - .
08:24 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 1 - .
Payload: Progress s/n 102. Mass: 7,020 kg (15,470 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 26.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 18.73 days. Completed Operations Date: 1978-02-08 02:00:20 . Decay Date: 1978-02-08 02:00:20 . USAF Sat Cat: 10603 . COSPAR: 1978-008A. Apogee: 256 km (159 mi). Perigee: 173 km (107 mi). Inclination: 51.60 deg. Period: 88.70 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 22 Jan 1978 10:12:14 GMT. Undocked on 6 Feb 1978 05:54:00 GMT. Destroyed in reentry on 8 Feb 1978 02:00:00 GMT. Total free-flight time 3.91 days. Total docked time 14.82 days.
1978 March 2 - .
15:28 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1978 March 10 - .
1978 March 16 - .
1978 April 4 - .
15:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1001 - .
Payload: Soyuz T s/n 4L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 10.87 days. Decay Date: 1978-04-15 . USAF Sat Cat: 10783 . COSPAR: 1978-036A. Apogee: 228 km (141 mi). Perigee: 199 km (123 mi). Inclination: 51.60 deg. Period: 88.70 min.
Manned precursor. Recovered April 15, 1978 12:02 GMT. Unsuccessful mission. Soyuz T test -failure.
Maneuver Summary:
202 km X 231 km orbit to 195 km X 291 km orbit. Delta V: 19 m/s
195 km X 291 km orbit to 306 km X 322 km orbit. Delta V: 40 m/s
306 km X 322 km orbit to 308 km X 318 km orbit. Delta V: 1 m/s
Total Delta V: 60 m/s.
Officially: Investigation of the upper atmosphere and outer space.
1978 June 15 - .
20:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 29 - .
Call Sign: Foton (Photon). Crew: Ivanchenkov,
Kovalyonok.
Backup Crew: Lyakhov,
Ryumin.
Payload: Soyuz 7K-T s/n 46. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 29.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 79.64 days. Decay Date: 1978-09-03 . USAF Sat Cat: 10952 . COSPAR: 1978-061A. Apogee: 248 km (154 mi). Perigee: 193 km (119 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Placed on board the Salyut-6 station a crew consisting of V.V. Kovalenko and A.S. Ivanchenkov to conduct scientific and technological investigations and experiments..
1978 June 27 - .
15:27 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 30 - .
Call Sign: Kavkas (Caucasus ). Crew: Hermaszewski,
Klimuk.
Backup Crew: Jankowski,
Kubasov.
Payload: Soyuz 7K-T(A9) s/n 67. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 29,
Soyuz 30.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T/A9.
Duration: 7.92 days. Decay Date: 1978-07-05 . USAF Sat Cat: 10968 . COSPAR: 1978-065A. Apogee: 244 km (151 mi). Perigee: 194 km (120 mi). Inclination: 51.60 deg. Period: 88.80 min. Manned two crew. Docked with Salyut 6. Placed on board the Salyut-6 station, under the Intercosmos programme, a second, international, crew consisting of P.I. Klimuk (USSR) and M. Hermaszewski (Poland) to conduct scientific investigations and experiments..
1978 July 5 - .
1978 July 7 - .
11:26 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 2 - .
Payload: Progress s/n 101. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 29.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 27.59 days. Completed Operations Date: 1978-08-04 01:30:51 . Decay Date: 1978-08-04 01:30:51 . USAF Sat Cat: 10979 . COSPAR: 1978-070A. Apogee: 307 km (190 mi). Perigee: 248 km (154 mi). Inclination: 51.60 deg. Period: 90.00 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 9 Jul 1978 12:58:59 GMT. Undocked on 2 Aug 1978 04:57:44 GMT. Destroyed in reentry on 4 Aug 1978 01:31:07 GMT. Total free-flight time 3.92 days. Total docked time 23.67 days.
1978 July 29 - .
04:00 GMT - .
1978 August 7 - .
22:31 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 3 - .
Payload: Progress s/n 103. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 29.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 15.76 days. Completed Operations Date: 1978-08-24 16:44:38 . Decay Date: 1978-08-24 16:44:38 . USAF Sat Cat: 10999 . COSPAR: 1978-077A. Apogee: 232 km (144 mi). Perigee: 190 km (110 mi). Inclination: 51.60 deg. Period: 88.70 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 9 Aug 1978 23:59:30 GMT. Undocked on 21 Aug 1978 15:42:50 GMT. Destroyed in reentry on 23 Aug 1978 16:45:00 GMT. Total free-flight time 4.10 days. Total docked time 11.66 days.
1978 August 20 - .
- Kamanin in Star City. - .
Nation: Russia.
Related Persons: Ivanchenkov,
Kovalyonok,
Yeliseyev.
Program: Salyut 6.
Flight: Soyuz 29.
At a visit to Star City, Kamanin is allowed to participate together with Yeliseyev in a communications session with the EO-2 crew (Ivanchenkov, Kovalyonok) aboard Salyut 6..
1978 August 26 - .
14:51 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 31 - .
Call Sign: Yastreb (Hawk ). Crew: Bykovsky,
Jaehn.
Backup Crew: Gorbatko,
Koellner.
Payload: Soyuz 7K-T s/n 47. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 29,
Soyuz 31.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 67.84 days. Decay Date: 1978-11-02 . USAF Sat Cat: 11010 . COSPAR: 1978-081A. Apogee: 243 km (150 mi). Perigee: 193 km (119 mi). Inclination: 51.60 deg. Period: 88.80 min. Manned two crew. Docked with Salyut 6. Delivered to the Salyut-6 station the third international 'Intercosmos' crew consisting of V F Bykovsky (USSR) and S Jaehn (German Democratic Republic) to carry out scientific research and experiments..
1978 September 3 - .
1978 October 3 - .
23:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 4 - .
Payload: Progress s/n 105. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 29.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 22.72 days. Completed Operations Date: 1978-10-27 16:27:43 . Decay Date: 1978-10-27 16:27:43 . USAF Sat Cat: 11040 . COSPAR: 1978-090A. Apogee: 247 km (153 mi). Perigee: 185 km (114 mi). Inclination: 51.70 deg. Period: 88.80 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 6 Oct 1978 01:00:15 GMT. Undocked on 24 Oct 1978 13:01:52 GMT. Destroyed in reentry on 26 Oct 1978 16:28:13 GMT. Total free-flight time 4.22 days. Total docked time 18.50 days.
1978 November 2 - .
1979 January 31 - .
09:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Cosmos 1074 - .
Payload: Soyuz T s/n 5L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 60.04 days. Decay Date: 1979-04-01 . USAF Sat Cat: 11259 . COSPAR: 1979-008A. Apogee: 238 km (147 mi). Perigee: 195 km (121 mi). Inclination: 51.60 deg. Period: 88.80 min.
Manned precursor. Recovered April 1, 1979 10:09 GMT. Soyuz T Test.
Maneuver Summary:
197 km X 240 km orbit to 255 km X 297 km orbit. Delta V: 33 m/s
255 km X 297 km orbit to 264 km X 306 km orbit. Delta V: 4 m/s
264 km X 306 km orbit to 309 km X 321 km orbit. Delta V: 17 m/s
309 km X 321 km orbit to 279 km X 357 km orbit. Delta V: 18 m/s
279 km X 357 km orbit to 352 km X 402 km orbit. Delta V: 32 m/s
352 km X 402 km orbit to 363 km X 384 km orbit. Delta V: 8 m/s
Total Delta V: 112 m/s
Officially: Investigation of the upper atmosphere and outer space.
1979 February 25 - .
11:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 32 - .
Call Sign: Proton (Proton ). Crew: Lyakhov,
Ryumin.
Backup Crew: Lebedev,
Popov.
Payload: Soyuz 7K-T s/n 48. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 32.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 110.18 days. Decay Date: 1979-06-13 . USAF Sat Cat: 11281 . COSPAR: 1979-018A. Apogee: 256 km (159 mi). Perigee: 193 km (119 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Transported a team consisting of V A Lyakhov and V V Ryumin to the Salyut-6 space station to conduct scientific investigations and experiments and repair work. Recovered June 15, 1979 16:18 GMT. Returned unmanned..
1979 March 12 - .
05:47 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 5 - .
Payload: Progress s/n 104. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 32.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 23.77 days. Completed Operations Date: 1979-04-05 00:09:54 . Decay Date: 1979-04-05 00:09:54 . USAF Sat Cat: 11292 . COSPAR: 1979-022A. Apogee: 256 km (159 mi). Perigee: 183 km (113 mi). Inclination: 51.70 deg. Period: 88.80 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 14 Mar 1979 07:19:21 GMT. Undocked on 3 Apr 1979 16:10:00 GMT. Destroyed in reentry on 5 Apr 1979 00:10:22 GMT. Total free-flight time 3.40 days. Total docked time 20.37 days.
1979 April 10 - .
17:34 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 33 - .
Call Sign: Saturn (Saturn ). Crew: Ivanov, Georgi,
Rukavishnikov.
Backup Crew: Aleksandrov, Aleksandr,
Romanenko.
Payload: Soyuz 7K-T s/n 49. Mass: 6,860 kg (15,120 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 32,
Soyuz 33.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 1.96 days. Decay Date: 1979-04-12 . USAF Sat Cat: 11324 . COSPAR: 1979-029A. Apogee: 261 km (162 mi). Perigee: 194 km (120 mi). Inclination: 51.60 deg. Period: 89.00 min. Manned two crew. Flight under the Intercosmos programme of an international team consisting of N N Rukavishnikov (USSR) and G I Ivanov (Bulgaria). Unsuccessful mission. Failed to rendezvous with Salyut 6..
1979 April 12 - .
1979 May 13 - .
04:17 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 6 - .
Payload: Progress s/n 106. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 32.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 27.61 days. Completed Operations Date: 1979-06-09 18:52:36 . Decay Date: 1979-06-09 18:52:36 . USAF Sat Cat: 11356 . COSPAR: 1979-039A. Apogee: 247 km (153 mi). Perigee: 190 km (110 mi). Inclination: 51.60 deg. Period: 88.80 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 15 May 1979 06:19:22 GMT. Undocked on 8 Jun 1979 07:59:41 GMT. Destroyed in reentry on 9 Jun 1979 18:52:46 GMT. Total free-flight time 3.54 days. Total docked time 24.07 days.
1979 June 6 - .
18:12 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1979 June 15 - .
1979 June 28 - .
09:25 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Progress 7 - .
Payload: Progress s/n 107. Mass: 7,014 kg (15,463 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned logistics spacecraft. Flight: Soyuz 32.
Spacecraft Bus: Soyuz.
Spacecraft: Progress.
Duration: 21.69 days. Completed Operations Date: 1979-07-20 01:57:19 . Decay Date: 1979-07-20 01:57:19 . USAF Sat Cat: 11421 . COSPAR: 1979-059A. Apogee: 251 km (155 mi). Perigee: 186 km (115 mi). Inclination: 51.60 deg. Period: 88.80 min.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 30 Jun 1979 11:18:22 GMT. Undocked on 18 Jul 1979 03:49:55 GMT. Destroyed in reentry on 20 Jul 1979 01:57:30 GMT. Total free-flight time 4.0 days. Total docked time 17.69 days.
- KRT-10 - .
Payload: KRT-10. Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Flight: Soyuz 32.
Spacecraft: KRT-10.
Decay Date: 1979-08-26 . USAF Sat Cat: 11493 . COSPAR: 1977-097BD. Apogee: 385 km (239 mi). Perigee: 359 km (223 mi). Inclination: 51.60 deg. Period: 91.99 min. 10 m diameter radio telescope. Attached to Salyut 6 docking hatch and deployed after separation of Progress from Mir..
1979 August 15 - .
14:16 GMT - .
1979 August 19 - .
1979 December 16 - .
12:29 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-1 - .
Payload: Soyuz T s/n 6L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 100.38 days. Decay Date: 1980-03-25 . USAF Sat Cat: 11640 . COSPAR: 1979-103A. Apogee: 252 km (156 mi). Perigee: 213 km (132 mi). Inclination: 51.60 deg. Period: 89.20 min.
New generation Soyuz capsule; unmanned flight to Salyut 6. Docked with Salyut 6. Recovered March 25, 1980 21:47 GMT. Unmanned test of Soyuz T design.
Officially: Complex experimental testing of new on-board systems and assemblies under various flight conditions and operation in conjunction with the Salyut-6 orbital station.
1980 March 27 - .
18:53 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1980 April 9 - .
13:38 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 35 - .
Call Sign: Dnepr (Dnieper ). Crew: Popov,
Ryumin.
Backup Crew: Andreyev,
Zudov.
Payload: Soyuz 7K-T s/n 51. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 55.06 days. Decay Date: 1980-06-03 . USAF Sat Cat: 11753 . COSPAR: 1980-027A. Apogee: 247 km (153 mi). Perigee: 197 km (122 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Carried crew comprising L I Popov and V V Ryumin to the Salyut-6 station to carry out scientific and technical research and experiments..
1980 April 27 - .
06:24 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1980 May 26 - .
18:20 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 36 - .
Call Sign: Orion (Orion ). Crew: Farkas,
Kubasov.
Backup Crew: Dzhanibekov,
Magyari.
Payload: Soyuz 7K-T s/n 52. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35,
Soyuz 36.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 65.87 days. Decay Date: 1980-07-31 . USAF Sat Cat: 11811 . COSPAR: 1980-041A. Apogee: 263 km (163 mi). Perigee: 190 km (110 mi). Inclination: 51.60 deg. Period: 89.00 min. Transported the fifth international crew under the INTERCOSMOS programme, comprising V N Kubasov (USSR) and B Farkas (Hungary) to the Salyut-6 station to carry out scientific research and experiments..
1980 June 3 - .
1980 June 5 - .
14:19 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-2 - .
Call Sign: Yupiter (Jupiter ). Crew: Aksyonov,
Malyshev.
Backup Crew: Kizim,
Makarov.
Payload: Soyuz T s/n 7L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35,
Soyuz T-2.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 3.93 days. Decay Date: 1980-06-09 . USAF Sat Cat: 11825 . COSPAR: 1980-045A. Apogee: 232 km (144 mi). Perigee: 195 km (121 mi). Inclination: 51.60 deg. Period: 88.70 min. Test flight of new Soyuz T; docked with Salyut 6. Conducted testing and development of on-board systems in the improved Soyuz T series transport vehicle under piloted conditions..
1980 June 9 - .
1980 June 29 - .
04:40 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1980 July 23 - .
18:33 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 37 - .
Call Sign: Terek (Terek - river in the Caucasus). Crew: Gorbatko,
Tuan.
Backup Crew: Bykovsky,
Liem.
Payload: Soyuz 7K-T s/n 53. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35,
Soyuz 37.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 79.64 days. Decay Date: 1980-10-11 . USAF Sat Cat: 11905 . COSPAR: 1980-064A. Apogee: 273 km (169 mi). Perigee: 190 km (110 mi). Inclination: 51.50 deg. Period: 89.10 min.
Manned two crew. Transported to the Salyut-6 station the sixth international crew under the Intercosmos programme, comprising V V Gorbatko (USSR) and Pham Tuan (Viet Nam), to conduct scientific research and experiments. Returned crew of Soyuz 35 to Earth. Recovered October 11, 1980 9:50 GMT.
1980 July 31 - .
1980 September 18 - .
19:11 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 38 - .
Call Sign: Taimyr (Taimyr - Russian peninsula). Crew: Romanenko,
Tamayo Mendez.
Backup Crew: Khrunov,
Lopez Falcon.
Payload: Soyuz 7K-T s/n 54. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 35,
Soyuz 38.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 7.86 days. Decay Date: 1980-09-26 . USAF Sat Cat: 11977 . COSPAR: 1980-075A. Apogee: 257 km (159 mi). Perigee: 195 km (121 mi). Inclination: 51.60 deg. Period: 89.00 min. Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 station the seventh international crew under the INTERCOSMOS programme, comprising Y V Romanenko (USSR) and A. Tomaio Mendez (Cuba), to conduct scientific research and experiments..
1980 September 26 - .
1980 September 28 - .
15:09 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1980 October 11 - .
1980 November - .
1980 November 27 - .
14:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-3 - .
Call Sign: Mayak (Beacon ). Crew: Kizim,
Makarov,
Strekalov.
Backup Crew: Kovalyonok,
Polyakov,
Savinykh.
Payload: Soyuz T s/n 8L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-3.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 12.80 days. Decay Date: 1980-12-10 . USAF Sat Cat: 12077 . COSPAR: 1980-094A. Apogee: 260 km (160 mi). Perigee: 256 km (159 mi). Inclination: 51.60 deg. Period: 89.70 min.
Manned three crew. Docked with Salyut 6. Tested the improved transport ship of the 'SOYUZ T' series; transported to the Salyut-6 orbital station a crew consisting of L D Kizim, O G Makarov and G M Strekalov to carry out repair and preventive work and scientific and technical investigation and experiments.
1980 December 10 - .
1981 January 24 - .
14:18 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1981 March 12 - .
19:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz T-4 - .
Call Sign: Foton (Photon ). Crew: Kovalyonok,
Savinykh.
Backup Crew: Andreyev,
Zudov.
Payload: Soyuz T s/n 10L. Mass: 6,850 kg (15,100 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz T-4.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz T.
Duration: 74.73 days. Decay Date: 1981-05-26 . USAF Sat Cat: 12334 . COSPAR: 1981-023A. Apogee: 237 km (147 mi). Perigee: 201 km (124 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station cosmonauts V V Kovalenok and V P Savinykh to carry out repairs and preventive maintenance and scientific and technical investigations and experiments..
1981 March 22 - .
14:58 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
1981 March 30 - .
1981 May 14 - .
17:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Soyuz-U.
- Soyuz 40 - .
Call Sign: Dnepr (Dnieper ). Crew: Popov,
Prunariu.
Backup Crew: Dediu,
Romanenko.
Payload: Soyuz 7K-T s/n 56. Mass: 6,800 kg (14,900 lb). Nation: Russia.
Agency: MOM.
Program: Salyut 6.
Class: Manned.
Type: Manned spacecraft. Flight: Soyuz 40,
Soyuz T-4.
Spacecraft Bus: Soyuz.
Spacecraft: Soyuz 7K-T.
Duration: 7.86 days. Decay Date: 1981-05-22 . USAF Sat Cat: 12454 . COSPAR: 1981-042A. Apogee: 270 km (160 mi). Perigee: 192 km (119 mi). Inclination: 51.60 deg. Period: 89.10 min. Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station the ninth international crew under the INTERCOSMOS programme, comprising L I Popov (USSR), and D. Prunariu (Romania), to conduct scientific research and experiments..
1981 May 22 - .
1981 May 26 - .
1982 July 29 - .
- Burnup of Salyut 6 Space Station (USSR) - .
Nation: Russia.
Spacecraft Bus: Almaz.
Spacecraft: Salyut 6.
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