|Mission type||Dock with Salyut 1|
|Operator||Soviet space program|
|Mission duration||1 day 23 hours 45 minutes 54 seconds|
|Spacecraft||Soyuz 7K-OKS No.1|
|Spacecraft type||Soyuz 7K-OKS|
|Manufacturer||Experimental Design Bureau (OKB-1)|
|Launch mass||6525 kg |
|Landing mass||1200 kg|
|Callsign||Гранит (Granit - "Granite") |
|Start of mission|
|Launch date||22 April 1971, 23:54:06 GMT|
|Launch site||Baikonur, Site 1/5 |
|End of mission|
|Landing date||24 April 1971, 23:40:00 GMT|
|Landing site||120 km at the northwest of Karaganda, Kazakhstan|
|Reference system||Geocentric orbit |
|Regime||Low Earth orbit|
|Perigee altitude||208.0 km|
|Apogee altitude||246.0 km|
Soyuz 10 mission patch
Soyuz 10 (Russian: 'Союз 10', Union 10) was launched on 22 April 1971 as the world's first mission to the world's first space station, the Soviet Salyut 1. The docking was not successful and the crew returned to Earth without having entered the station. It would be the first of numerous docking failures in the Soviet space station program.
The cosmonauts Vladimir Shatalov, Aleksei Yeliseyev, and Nikolai Rukavishnikov were able to navigate their Soyuz 10 spacecraft to the Salyut 1 station, yet during docking they ran into problems. The automatic control system failed during approach, owing to a serious design oversight. Soft dock (contact between the spacecraft and station without a full link) was achieved on 24 April 1971 at 01:47 GMT, but the computer sensed an abnormality in the spacecraft's alignment and began firing the attitude control jets to compensate. With Soyuz 10 being pushed to one side by the attitude control system, it became impossible to achieve hard dock, and large quantities of propellant were expended doing so. The docking attempt was called off, but further difficulty occurred when the probe would not come out of the space station's docking cone. The obvious solution was simply to jettison the orbital module and leave it attached to Salyut 1, but this would make it impossible for future Soyuz missions to dock; thus, the space station would have to be abandoned. Eventually, ground controllers realised that the cosmonauts could throw a circuit breaker in the docking mechanism, for interrupting the power supply would cause the probe to automatically retract. This procedure worked, and undocking was completed and the capsule returned to Earth later on 24 April 1971 at 23:40 GMT. The automatic control system would be redesigned on future Soyuz spacecraft.
Third and last spaceflight
|Flight Engineer||Aleksei Yeliseyev|
Third and last spaceflight
|Systems Engineer ||Nikolai Rukavishnikov|
|Flight Engineer||Valeri Kubasov|
|Systems Engineer||Pyotr Kolodin|
|Flight Engineer||Vladislav Volkov|
|Systems Engineer||Viktor Patsayev|
- Mass: 6,525 kg (14,385 lb) 
- Perigee: 208.0 km (129.2 mi) 
- Apogee: 246.0 km (152.9 mi)
- Inclination: 51.6°
- Period: 89.0 minutes
Retrorockets were fired at the first opportunity after undocking to permit return to Earth. One last hitch presented itself when toxic fumes began to fill the capsule during reentry, causing Rukavishnikov to pass out; however, all three crew members were recovered unscathed. The landing at 120 km at the northwest of Karaganda, Kazakhstan, the first (pre-dawn) landing of a crewed spacecraft, was a success.
- Soyuz T-13, a mission to manually dock to the crippled Salyut 7 space station
- Soyuz T-15, a mission to ferry equipment from Salyut 7 to Mir, which had to manually maneuver and dock to Mir
- "Display: Soyuz 10 1971-034A". NASA. 14 May 2020. Retrieved 18 October 2020. This article incorporates text from this source, which is in the public domain.
- Mir Hardware Heritage - 1.7.3 (wikisource)
- "Baikonur LC1". Encyclopedia Astronautica. Archived from the original on 15 April 2009. Retrieved 4 March 2009.
- "Trajectory: Soyuz 10 1971-034A". NASA. 14 May 2020. Retrieved 18 October 2020. This article incorporates text from this source, which is in the public domain.
- The mission report is available here: http://www.spacefacts.de/mission/english/soyuz-10.htm