Progress M-14
A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1992-055A |
| SATCAT no. | 22090 |
| Spacecraft properties | |
| Spacecraft | Progress M-14 (No.209) |
| Spacecraft type | Progress-M-VDU 11F615A55 |
| Manufacturer | NPO Energia |
| Start of mission | |
| Launch date | 15 August 1992, 22:18:32 UTC |
| Rocket | Soyuz-U2 |
| Launch site | Baikonur 31/6 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 21 October 1992, 23:12:00 GMT |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 187 kilometres (116 mi) |
| Apogee altitude | 221 kilometres (137 mi) |
| Inclination | 51.5 degrees |
| Period | 88.6 minutes |
| Docking with Mir | |
| Docking port | Kvant-1 Aft |
| Docking date | 18 August 1992, 00:20:48 UTC |
| Undocking date | 21 October 1992, 16:46:01 UTC |
| Time docked | 64.68 days |
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. Progress M-14 also carried the sixth VBK-Raduga capsule, which was recovered after the flight.