Soyuz TM-1

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Soyuz TM-1
COSPAR ID 1986-035A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 16722
Mission duration9 days
Spacecraft properties
Spacecraft type Soyuz-TM
Manufacturer NPO Energia
Launch mass6,450 kilograms (14,220 lb)
Start of mission
Launch date21 May 1986 (1986-05-21Z) UTC
Rocket Soyuz-U2
Launch site Baikonur 1/5
End of mission
Landing date30 May 1986 (1986-05-31Z) UTC
Orbital parameters
Reference system Geocentric
Regime Low Earth
Docking with Mir
Docking date23 May 1986
Undocking date29 May 1986
 

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. [1] It docked to Mir on 23 May 1986, and undocked on the 29th. [2] It was the last uncrewed Soyuz flight until Soyuz MS-14, in 2019.

Contents

Mission parameters

Related Research Articles

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Military Soyuz

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Soyuz-T

The Soyuz-T spacecraft was the third generation Soyuz spacecraft, in service for seven years from 1979 to 1986. The T stood for transport. The revised spacecraft incorporated lessons learned from the Apollo Soyuz Test Project, Soyuz 7K-TM and Military Soyuz.

Soyuz 7K-TM

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Igla (spacecraft docking system)

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References

  1. "Soyuz TM". Astronautix. Archived from the original on October 31, 2016. Retrieved 30 October 2016.
  2. "Soyuz TM-1". WorldSpaceFlight. Retrieved 11 February 2016.

Further reading