 A Progress 7K-TG spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1988-038A |
| SATCAT no. | 19117[1] |
| Spacecraft properties | |
| Spacecraft | Progress (No.144) |
| Spacecraft type | Progress 7K-TG[2] |
| Manufacturer | NPO Energia |
| Start of mission | |
| Launch date | 13 May 1988, 00:30:25 UTC[1] |
| Rocket | Soyuz-U2[2] |
| Launch site | Baikonur, Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 5 June 1988, 20:28:00 UTC[3] |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 185 km[3] |
| Apogee altitude | 246 km[3] |
| Inclination | 51.7°[3] |
| Period | 88.8 minutes[3] |
| Epoch | 13 May 1988 |
| Docking with Mir | |
| Docking port | Kvant-1 aft[3] |
| Docking date | 15 May 1988, 02:13:26 UTC |
| Undocking date | 5 June 1988, 11:11:55 UTC |
Progress 36 (Russian: Прогресс 36) was a Soviet uncrewed Progress cargo spacecraft, which was launched in May 1988 to resupply the Mir space station.
Launch
Progress 36 launched on 13 May 1988 from the Baikonur Cosmodrome in the Kazakh SSR. It used a Soyuz-U2 rocket.[2][4]
Docking
Progress 36 docked with the aft port of the Kvant-1 module of Mir on 15 May 1988 at 02:13:26 UTC, and was undocked on 5 June 1988 at 11:11:55 UTC.[3][5]
Decay
It remained in orbit until 5 June 1988, when it was deorbited. The deorbit burn occurred at 20:28:00 UTC and the mission ended at 21:18:40 UTC.[3][5]
See also
References
- ^ a b "Launchlog". Jonathan's Space Report. Retrieved 6 December 2020.
- ^ a b c "Progress 1 - 42 (11F615A15, 7K-TG)". Gunter's Space Page. Retrieved 6 December 2020.
- ^ a b c d e f g h "Cargo spacecraft "Progress 36"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.
- ^ "Progress 36". NASA. Retrieved 6 December 2020.
This article incorporates text from this source, which is in the public domain.
- ^ a b "Mir". Astronautix. Archived from the original on 20 August 2016. Retrieved 6 December 2020.
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