Mission type | Mir resupply |
---|---|
COSPAR ID | 1992-055A |
SATCAT no. | 22090 [1] |
Spacecraft properties | |
Spacecraft | Progress M-14 (No.209) |
Spacecraft type | Progress-M-VDU 11F615A55 [2] |
Manufacturer | NPO Energia |
Start of mission | |
Launch date | 15 August 1992, 22:18:32[1] | UTC
Rocket | Soyuz-U2 [2] |
Launch site | Baikonur 31/6 [2] |
End of mission | |
Disposal | Deorbited |
Decay date | 21 October 1992, 23:12:00[3] | GMT
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 187 kilometres (116 mi) [4] |
Apogee altitude | 221 kilometres (137 mi) [4] |
Inclination | 51.5 degrees [4] |
Period | 88.6 minutes [4] |
Docking with Mir | |
Docking port | Kvant-1 Aft |
Docking date | 18 August 1992, 00:20:48 UTC [4] |
Undocking date | 21 October 1992, 16:46:01 UTC [4] |
Time docked | 64.68 days [3] |
Progress M-14 ( Russian: Прогресс M-14), was a Russian uncrewed Progress cargo spacecraft which was launched in 1992 to resupply the Mir space station. The spacecraft was modified to transport the first VDU propulsion unit to Mir. [3] Progress M-14 also carried the sixth VBK-Raduga capsule, [5] which was recovered after the flight.
Progress M-14 launched on 15 August 1992 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U2 rocket. [2]
Progress M-14 docked with Mir on 18 August 1992 at 00:20:48 GMT. [3]