Progress M-24
A Progress-M spacecraft | |
| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1994-052A |
| SATCAT no. | 23215 |
| Spacecraft properties | |
| Spacecraft type | Progress-M 11F615A55 |
| Manufacturer | NPO Energia |
| Launch mass | 7,250 kilograms (15,980 lb) |
| Start of mission | |
| Launch date | 25 August 1994, 14:25:12 UTC |
| Rocket | Soyuz-U |
| Launch site | Baikonur Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 4 October 1994, 22:43 UTC |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Inclination | 51.6 degrees |
| Docking with Mir | |
| Docking port | Core Forward |
| Docking date | 2 September 1994, 13:30:28 UTC |
| Undocking date | 4 October 1994, 18:55:52 UTC |
| Time docked | 32.2 days |
Progress M-24 (Russian: Прогресс М-24) was a Russian uncrewed cargo spacecraft which was launched in 1994 to resupply the Mir space station; causing minor damage to the station as the result of a collision during a failed attempt to dock.