Progress M-36
Appearance
Mission type | Mir resupply |
---|---|
COSPAR ID | 1997-058A |
SATCAT no. | 25002[1] |
Spacecraft properties | |
Spacecraft | Progress (No.236) |
Spacecraft type | Progress-M[2] |
Manufacturer | RKK Energia |
Start of mission | |
Launch date | 5 October 1997, 15:08:57 UTC[1] |
Rocket | Soyuz-U[2] |
Launch site | Baikonur, Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 19 December 1997, 13:20:01 UTC[3] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 193 km[3] |
Apogee altitude | 246 km[3] |
Inclination | 51.6°[3] |
Period | 88.6 minutes[3] |
Epoch | 5 October 1997 |
Docking with Mir | |
Docking port | Kvant-1 aft[3] |
Docking date | 8 October 1997, 17:07:09 UTC |
Undocking date | 17 December 1997, 06:01:53 UTC |
Progress M-36 (Russian: Прогресс M-36) was a Russian unmanned Progress cargo spacecraft, which was launched in October 1997 to resupply the Mir space station.
Launch
[edit]Progress M-36 launched on 5 October 1997 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket.[2][4]
Docking
[edit]Progress M-36 docked with the aft port of the Kvant-1 module of Mir on 8 October 1997 at 17:07:09 UTC, and was undocked on 17 December 1997 at 06:01:53 UTC.[3][5]
Decay
[edit]It remained in orbit until 19 December 1997, when it was deorbited. The deorbit burn occurred at 13:20:01 UTC, with the mission ending at 13:59:01 UTC.[3][5]
See also
[edit]References
[edit]- ^ a b "Launchlog". Jonathan's Space Report. Retrieved 3 December 2020.
- ^ a b c "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 3 December 2020.
- ^ a b c d e f g h "Cargo spacecraft "Progress M-36"". Manned Astronautics figures and facts. Archived from the original on 9 October 2007.
- ^ "Progress M-36". NASA. Retrieved 3 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 3 December 2020.