Progress M-SO1
![]() Progress M-SO1 approaching the ISS with Pirs | |
Mission type | ISS assembly |
---|---|
Operator | Roskosmos |
COSPAR ID | 2001-041A |
Spacecraft properties | |
Spacecraft type | Progress (modified) |
Manufacturer | RKK Energia |
Start of mission | |
Launch date | 14 September 2001, 23:34:55 UTC |
Rocket | Soyuz-U |
Launch site | Baikonur Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 27 September 2001, 00:01 UTC |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Inclination | 51.6 degrees |
Docking with ISS | |
Docking port | Zvezda Nadir (Pirs) |
Docking date | 17 September 2001, 01:05 UTC |
Undocking date | 26 September 2001, 15:36 UTC |
Time docked | 9½ days |
Payload | |
Pirs |
Progress M-SO1 was a modified Progress spacecraft used to deliver the Pirs module to the International Space Station.[1] It was based on the Progress-M 11F615A55 spacecraft, with the pressurised cargo module removed to accommodate Pirs, and had the serial number 301.[2]
Progress M-SO1 was launched by a Soyuz-U carrier rocket from Site 1/5 at the Baikonur Cosmodrome. Launch occurred at 23:34:55 GMT on 14 September 2001.[2] The spacecraft docked with the Nadir port of the Zvezda module at 01:05 GMT on 17 September.[3] It remained docked for nine and a half days before it was jettisonned from Pirs at 15:36 GMT on 26 September. It was deorbited at 23:30 GMT on the same day, and burned up in the atmosphere over the Pacific Ocean, with any remaining debris landing in the ocean at around 00:01 GMT on 27 September.[4]
See also
References
- ↑ Zak, Anatoly. "Progress cargo ship". RussianSpaceWeb. Retrieved 2009-06-07.
- 1 2 McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-06-07.
- ↑ Wade, Mark. "Progress M-SO". Encyclopedia Astronautica. Retrieved 2009-06-07.
- ↑ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 2009-06-07.