| Mission type | Mir resupply |
|---|---|
| COSPAR ID | 1993-019A |
| SATCAT no. | 22588 |
| Spacecraft properties | |
| Spacecraft type | Progress-M 11F615A55 |
| Manufacturer | NPO Energia |
| Launch mass | 7,250 kilograms (15,980 lb) |
| Start of mission | |
| Launch date | 31 March 1993, 03:34:13 UTC |
| Rocket | Soyuz-U2 |
| Launch site | Baikonur Site 1/5 |
| End of mission | |
| Disposal | Deorbited |
| Decay date | 3 March 1994, 03:28 UTC |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 391 kilometres (243 mi)[1] |
| Apogee altitude | 391 kilometres (243 mi)[1] |
| Inclination | 51.6 degrees |
| Docking with Mir | |
| Docking port | Kvant-1 Aft |
| Docking date | 1 April 1993, 05:16:18 UTC |
| Undocking date | 11 August 1993, 15:36:42 UTC |
| Time docked | 132 days |
Progress Mir Resupply | |
Progress M-17 (Russian: Прогресс М-17) was a Russian uncrewed cargo spacecraft which was launched in 1993 to resupply the Mir space station.[2] The thirty-fifth of sixty-four Progress spacecraft to visit Mir, it used the Progress-M 11F615A55 configuration,[3] and had the serial number 217.[4] In addition to delivering cargo, Progress M-17 was also used to demonstrate extended duration Progress missions; remaining in orbit for almost a year with a docked phase lasting 132 days.
- ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 21 November 2010.
- ^ "Progress M-17". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 21 November 2010.
- ^ Krebs, Gunter. "Progress-M 1 - 13, 15 - 37, 39 - 67 (11F615A55, 7KTGM)". Gunter's Space Page. Retrieved 21 November 2010.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 21 November 2010.