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Soyuz 15

1974 Soviet crewed spaceflight to Salyut 3


1974 Soviet crewed spaceflight to Salyut 3

FieldValue
nameSoyuz 15
imageSoyuz 7K-T 2-seats drawing.svg
image_size300px
mission_typeSalyut 3 crew transport
operatorSoviet space program
COSPAR_ID1974-067A
SATCAT7421
mission_duration
orbits_completed32
spacecraftSoyuz 7K-T No.4
spacecraft_typeSoyuz 7K-T/A9
manufacturerOKB-1
launch_mass6570 kg
landing_mass1200 kg
launch_date26 August 1974, 19:58:05 UTC
launch_rocketSoyuz 11A511
launch_siteBaikonur 1/5
landing_date28 August 1974, 20:10:16 UTC
landing_site48 km at the southwest of Tselinograd
crew_size2
crew_membersGennady Sarafanov
Lev Dyomin
crew_callsignДунай (Dunay - "Danube")
crew_photoUSSR stamp Soyuz-15 1974 10k.jpg
crew_photo_captionSoviet stamp featuring Sarafanov and Dyomin (1974)
crew_photo_size300px
orbit_referenceGeocentric orbit
orbit_regimeLow Earth orbit
orbit_periapsis254 km
orbit_apoapsis275 km
orbit_inclination51.60°
orbit_period89.60 minutes
apsisgee
programmeSoyuz programme
previous_missionKosmos 672
next_missionSoyuz 16

Lev Dyomin

Soyuz 15 (, Union 15) was an August 1974 crewed 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 Gennady Sarafanov and Lev Dyomin 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 1974. 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.

Crew

Backup crew

Reserve crew

Mission parameters

  • Mass: 6570 kg
  • Perigee: 254.0 km
  • Apogee: 275.0 km
  • Inclination: 51.60°
  • Period: 89.60 minutes

References

References

  1. "Baikonur LC1". Encyclopedia Astronautica.
  2. Clark, Phillip. (1988). "The Soviet Manned Space Program". Orion Books, a division of Crown Publishers, Inc..
  3. Newkirk, Dennis. (1990). "Almanac of Soviet Manned Space Flight". Gulf Publishing Company.
  4. (14 May 2020). "Display: Soyuz 15 1974-067A". NASA.
  5. (14 May 2020). "Trajectory: Soyuz 15 1974-067A". NASA.
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