This article is about the 1974 mission.
For the mission identified by NASA as ISS Soyuz 15, see
Soyuz TMA-11.
Soyuz 15
|
Mission duration |
2 days, 12 minutes, 11 seconds |
---|
Orbits completed |
32 |
---|
|
Spacecraft properties |
---|
Spacecraft type |
Soyuz 7K-T/A9 |
---|
Manufacturer |
NPO Energia |
---|
Launch mass |
6,760 kilograms (14,900 lb) |
---|
|
Crew |
---|
Crew size |
2 |
---|
Members |
Gennadi Sarafanov Lev Dyomin |
---|
Callsign |
Дунай (Dunay - "Danube") |
---|
|
Start of mission |
---|
Launch date |
August 26, 1974, 19:58:05 (1974-08-26UTC19:58:05Z) UTC |
---|
Rocket |
Soyuz |
---|
Launch site |
Baikonur 1/5[1] |
---|
|
End of mission |
---|
Landing date |
August 28, 1974, 20:10:16 (1974-08-28UTC20:10:17Z) UTC |
---|
Landing site |
48 kilometres (30 mi) SW of Tselinograd |
---|
|
Orbital parameters |
---|
Reference system |
Geocentric |
---|
Regime |
Low Earth |
---|
Perigee |
173 kilometres (107 mi) |
---|
Apogee |
236 kilometres (147 mi) |
---|
Inclination |
51.6 degrees |
---|
Period |
88.5 minutes |
---|
|
Soyuz 15 (Russian: Союз 15, Union 15) was a 1974 manned space flight which was to have been the second mission to the Soviet Union's Salyut 3 space station with presumably military objectives.[2]
Launched 26 August 1974, the Soyuz spacecraft arrived at the station, but cosmonauts Lev Dyomin and Gennadi Sarafanov were unable to dock because of a fault in the automated docking system. Without sufficient fuel for prolonged attempts at manual docking, the mission had to be abandoned.[3] The crew landed 28 August. Analysis of the launch window was cited by observers for concluding a flight of 19 to 29 days had been planned.[3]
It was later claimed by Soviet authorities that no docking had been intended and that the flight had been undertaken merely to develop techniques for maneuvering near the space station.[2] They also said that a new automatic docking system was tested which would be used on future Progress transport craft.[3]
Crew
Backup crew
Reserve crew
Mission parameters
- Mass: 6,760 kg (14,900 lb)
- Perigee: 173 km (107 mi)
- Apogee: 236 km (147 mi)
- Inclination: 51.6°
- Period: 88.5 min
References
- ↑ "Baikonur LC1". Encyclopedia Astronautica. Retrieved 2009-03-04.
- ↑ 2.0 2.1 Clark, Phillip (1988). The Soviet Manned Space Program. New York: Orion Books, a division of Crown Publishers, Inc. ISBN 0-517-56954-X.
- ↑ 3.0 3.1 3.2 Newkirk, Dennis (1990). Almanac of Soviet Manned Space Flight. Houston, Texas: Gulf Publishing Company. ISBN 0-87201-848-2.
|
---|
| Main topics | |
---|
| Unmanned missions | |
---|
| Manned missions |
|
---|
| Launch sites | |
---|
|