Rahul Sharma (Editor)

Soyuz 15

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COSPAR ID
  
1974-067A

Spacecraft type
  
Soyuz 7K-T/A9

Launch date
  
26 August 1974

Rocket
  
Soyuz

Orbits completed
  
32

Dates
  
26 Aug 1974 – 28 Aug 1974

Landing date
  
28 August 1974

Crew size
  
2

Soyuz 15 wwwspacefactsdemissionphotosoyuz15jpg

Mission duration
  
2 days, 12 minutes, 11 seconds

Launch mass
  
6,760 kilograms (14,900 lb)

Callsign
  
Дунай (Dunay - "Danube")

Manufacturer
  
S. P. Korolev Rocket and Space Corporation Energia

Members
  
Gennadi Sarafanov, Lev Dyomin

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.

Launched 26 August 1974, the Soyuz spacecraft arrived at the station, but cosmonauts Lev Dyomin and Gennadi Sarafanov were unable to dock because the electronics in the Igla docking system malfunctioned. Without sufficient fuel for prolonged attempts at manual docking, the mission had to be abandoned. The cosmonauts powered down all nonessential systems in the Soyuz and waited until the next day for reentry. 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.

In the event of the failure, official TASS statements merely claimed that the mission was intended to practice docking maneuvers with the Salyut 3 station. They also said that a new automatic docking system was tested which would be used on future Progress transport craft.

The failed mission exposed a number of serious design flaws in the Soyuz 7K-T spacecraft, namely its lack of reserve propellant and electrical power for repeated docking attempts. In addition, the Igla docking system was found to be in major need of improvement. Since it was impossible to carry out these changes before Salyut 3 finished its operating lifespan, they had to wait for future space stations. The backup spacecraft for the Soyuz 15 mission was placed in storage and later flown as Soyuz 20 despite being past its intended shelf life.

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

    Soyuz 15 Wikipedia


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