Soyuz TM-1

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Soyuz TM-1
Mission duration 9 days
Spacecraft properties
Spacecraft type Soyuz-TM
Manufacturer NPO Energia
Launch mass 6,450 kilograms (14,220 lb)
Start of mission
Launch date 21 May 1986 (1986-05-21Z) UTC
Rocket Soyuz-U2
Launch site Baikonur 1/5
End of mission
Landing date 30 May 1986 (1986-05-31Z) UTC
Orbital parameters
Reference system Geocentric
Regime Low Earth
Docking with Mir

Soyuz TM-1 was an unmanned test flight of the Soyuz-TM spacecraft, intended for use in the Mir space station program. This was the maiden flight of the Soyuz-TM spacecraft, intended as the successor to the Soyuz-T spacecraft used in the Salyut program.

Mission parameters[edit]

  • Spacecraft: Soyuz-7K-STM
  • Mass: 6450 kg
  • Crew: None
  • Launched: May 21, 1986
  • Landed: May 30, 1986

References[edit]

Further reading[edit]