Soyuz 12

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Soyuz 12
Mission typeTest flight
Operator Soviet space program
COSPAR ID 1973-067A
SATCAT no. 06836
Mission duration1 day 23 hours 15 minutes 32 seconds
Orbits completed31
Spacecraft properties
SpacecraftSoyuz 7K-T No.1
Spacecraft type Soyuz 7K-T
Manufacturer Experimental Design Bureau (OKB-1)
Launch mass6570 kg [1]
Landing mass1200 kg
Crew
Crew size2
Members Vasily Lazarev
Oleg Grigoryevich Makarov
CallsignУрал (Ural - "Ural")
Start of mission
Launch date27 September 1973,
12:18:16 UTC
Rocket Soyuz
Launch site Baikonur, Site 1/5 [2]
End of mission
Landing date29 September 1973, 11:33:48 UTC
Landing site400 km at the southwest of Karaganda, Kazakhstan
Orbital parameters
Reference system Geocentric orbit [3]
Regime Low Earth orbit
Perigee altitude 194.0 km
Apogee altitude 249.0 km
Inclination 51.6°
Period 88.6 minutes
Salyut program insignia.svg
Salyut program insignia
  Soyuz 11
Soyuz 13  
 

Soyuz 12 (Russian : Союз 12, Union 12) was a 1973 crewed test flight by the Soviet Union of the newly redesigned Soyuz 7K-T spacecraft that was intended to provide greater crew safety in the wake of the Soyuz 11 tragedy. The flight marked the return of the Soviets to crewed space operations after the 1971 accident. The crew capacity of the capsule had been decreased from three to two cosmonauts to allow for pressure suits to be worn during launch, re-entry and docking. It was the first time pressure suits were used for reentry since the Voskhod 2 flight. [4]

Contents

Cosmonauts Vasily Lazarev and Oleg Grigoryevich Makarov spent two days in space testing the new craft.

Crew

Position Cosmonaut
Commander Vasily Lazarev
First spaceflight
Flight Engineer Oleg Grigoryevich Makarov
First spaceflight

Backup crew

Position Cosmonaut
Commander Aleksei Gubarev
Flight Engineer Georgy Grechko

Reserve crew

Position Cosmonaut
Commander Pyotr Klimuk
Flight Engineer Vitaly Sevastyanov

Mission parameters

Mission highlights

As the first crewed test of the new version of the Soyuz ferry craft, Soyuz 12 was to have flown to a Salyut station. [4] But the failures of Salyut 2 (4 April 1973) and Cosmos 557 (11 May 1973) in the months previous meant there was no station for the craft to dock to. The service module had no solar panels, carrying batteries for power instead, which limited the flight to about two days, enough time for a journey to and from a space station. [4]

Cosmonauts Lazarev and Makarov wore pressure suits for launch and landing, and would have worn them for a station docking, all changes brought about by the Soyuz 11 tragedy. The bulk of the suits and their environmental control systems limited the crew size to two. [4]

After the successful 27 September 1973 launch, the craft was maneuvered to a 326 x 344 km orbit on the second day in space, [4] which later proved to be the standard orbit for the Salyut 4 space station. A multispectral camera in the orbital module was used in coordination with aircraft to photograph the Earth. It was reported that the intention of the camera was to survey crop and forest conditions [4] The cosmonauts also utilised the Molniya 1 satellite to communicate with ground stations when out of range. [4] The crew landed safely on 29 September 1973 and the mission was called "flawless". [4] A large object was jettisoned when the craft was preparing for retrofire. The object remained in orbit for 116 days, landing at 400 km at the southwest of Karaganda, Kazakhstan. [4]

See also

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References

  1. 1 2 "Display: Soyuz 12 1973-067A". NASA. 14 May 2020. Retrieved 18 October 2020.PD-icon.svgThis article incorporates text from this source, which is in the public domain.
  2. "Baikonur LC1". Encyclopedia Astronautica. Archived from the original on 15 April 2009. Retrieved 4 March 2009.
  3. 1 2 "Trajectory: Soyuz 12 1973-067A". NASA. 14 May 2020. Retrieved 18 October 2020.PD-icon.svgThis article incorporates text from this source, which is in the public domain.
  4. 1 2 3 4 5 6 7 8 9 Newkirk, Dennis (1990). Almanac of Soviet Manned Space Flight. Houston, Texas: Gulf Publishing Company. ISBN   0-87201-848-2.