| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1991-073A |
| SATCATno. | 21746 |
| Spacecraft properties | |
| Spacecraft type | Progress-M 11F615A55 |
| Manufacturer | NPO Energia |
| Launch mass | 7,250 kilograms (15,980 lb) |
| Start of mission | |
| Launch date | 17 October 1991, 00:05:25 (1991-10-17UTC00:05:25Z) UTC |
| Rocket | Soyuz-U2 |
| Launch site | BaikonurSite 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 20 January 1992 (1992-01-21) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 376 kilometres (234 mi)[1] |
| Apogee altitude | 377 kilometres (234 mi)[1] |
| Inclination | 51.6 degrees |
| Docking withMir | |
| Docking port | Core Forward |
| Docking date | 21 October 1991, 03:40:50 UTC |
| Undocking date | 20 January 1992, 07:13:44 UTC |
| Time docked | 91 days |
Progress M-10 (Russian:Прогресс М-10) was a Soviet and subsequently Russianuncrewed cargo spacecraft which was launched in 1991 to resupply theMir space station.[2] The 28th of 64Progress spacecraft to visit Mir, it used theProgress-M 11F615A55 configuration,[3] and had theserial number 211.[4] It carried supplies including food, water, and oxygen for theEO-10 crew aboard Mir, as well as equipment for conducting scientific research, and fuel for adjusting the station's orbit and performing manoeuvres. It carried the fourthVBK-Raduga capsule, which was used to return experiment results and equipment to Earth when the Progress was deorbited.
Progress M-10 was launched at 00:05:25 GMT on 17 October 1991, atop aSoyuz-U2 carrier rocket flying fromSite 1/5 at theBaikonur Cosmodrome.[4] Following four days of free flight, it docked with the forward port of thecore module on the second attempt, at 03:40:50 GMT on 21 October.[5] The first attempt had been aborted by the Progress' onboard computer when the spacecraft was 150 metres (490 ft) away from the station.[6]
During the 91 days for which Progress M-10 was docked, Mir was in an orbit of around 376 by 377 kilometres (203 by 204 nmi),inclined at 51.6 degrees.[1] It was launched by the Soviet Union, whichwas dissolved in December 1991, and along with most aspects of theSoviet space programme, Progress M-10 was inherited by Russia. It undocked from Mir at 07:13:44 GMT on 20 January 1992, and was deorbited few hours later to a destructivereentry over thePacific Ocean.[1] The Raduga capsule landed at 12:03:30 GMT.[5]
