Soyuz TM-1
| COSPAR ID | 1986-035A |
|---|---|
| SATCATno. | 16722 |
| 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 1986UTC |
| Rocket | Soyuz-U2 |
| Launch site | Baikonur1/5 |
| End of mission | |
| Landing date | 30 May 1986UTC |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Docking withMir | |
| Docking date | 23 May 1986 |
| Undocking date | 29 May 1986 |
Soyuz TM-1was an unmanned test flight of theSoyuz-TMspacecraft, intended for use in theMirspace stationprogram. This was the maiden flight of the Soyuz-TM spacecraft, intended as the successor to theSoyuz-Tspacecraft used in theSalyut program.[1]It docked to Mir on 23 May 1986, and undocked on the 29th.[2]It was the last uncrewedSoyuzflight untilSoyuz MS-14,in 2019.
Mission parameters
[edit]- Spacecraft: Soyuz-7K-STM
- Mass: 6450 kg
- Crew: None
- Launched: May 21, 1986
- Landed: May 30, 1986
References
[edit]- ^"Soyuz TM".Astronautix. Archived fromthe originalon October 31, 2016.Retrieved30 October2016.
- ^"Soyuz TM-1".WorldSpaceFlight.Retrieved11 February2016.
Further reading
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