![]() A Progress-M spacecraft | |
Mission type | Mir resupply |
---|---|
COSPAR ID | 1996-043A |
SATCAT no. | 24071 [1] |
Spacecraft properties | |
Spacecraft | Progress (No.232) |
Spacecraft type | Progress-M [2] |
Manufacturer | RKK Energia |
Start of mission | |
Launch date | 31 July 1996, 20:00:06 UTC [1] |
Rocket | Soyuz-U [2] |
Launch site | Baikonur, Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 20 November 1996, 22:42:25 UTC [3] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 186 km [3] |
Apogee altitude | 229 km [3] |
Inclination | 51.6° [3] |
Period | 88.6 minutes [3] |
Epoch | 31 July 1996 |
Docking with Mir | |
Docking port | Mir Core Module forward [3] |
Docking date | 2 August 1996, 22:03:40 UTC |
Undocking date | 18 August 1996, 09:33:45 UTC |
Docking with Mir | |
Docking port | Kvant-1 aft [3] |
Docking date | 3 September 1996, 09:35:00 UTC |
Undocking date | 20 November 1996, 19:51:20 UTC |
Progress M-32 ( Russian: Прогресс M-32) was a Russian unmanned Progress cargo spacecraft, which was launched in July 1996 to resupply the Mir space station.
Progress M-32 launched on 31 July 1996 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket. [2] [4] The launch was postponed several times, primarily following problems with quality control during Soyuz-U production. [5]
Progress M-32 docked with the forward port of the Mir Core Module on 2 August 1996 at 22:03:40 UTC, and was undocked on 18 August 1996 at 09:33:45 UTC to make way for Soyuz TM-24. [5] [3] On 3 September 1996 at 09:35:00 UTC, Progress M-32 was redocked at the aft port of the Kvant-1 module of Mir, following the departure of Soyuz TM-23. Progress M-32 was finally undocked on 20 November 1996 at 19:51:20 UTC. [5] [3]
It remained in orbit until 20 November 1996, when it was deorbited. The deorbit burn occurred at 22:42:25 UTC. [5] [3]
![]() A Progress-M spacecraft | |
Mission type | Mir resupply |
---|---|
COSPAR ID | 1996-043A |
SATCAT no. | 24071 [1] |
Spacecraft properties | |
Spacecraft | Progress (No.232) |
Spacecraft type | Progress-M [2] |
Manufacturer | RKK Energia |
Start of mission | |
Launch date | 31 July 1996, 20:00:06 UTC [1] |
Rocket | Soyuz-U [2] |
Launch site | Baikonur, Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 20 November 1996, 22:42:25 UTC [3] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 186 km [3] |
Apogee altitude | 229 km [3] |
Inclination | 51.6° [3] |
Period | 88.6 minutes [3] |
Epoch | 31 July 1996 |
Docking with Mir | |
Docking port | Mir Core Module forward [3] |
Docking date | 2 August 1996, 22:03:40 UTC |
Undocking date | 18 August 1996, 09:33:45 UTC |
Docking with Mir | |
Docking port | Kvant-1 aft [3] |
Docking date | 3 September 1996, 09:35:00 UTC |
Undocking date | 20 November 1996, 19:51:20 UTC |
Progress M-32 ( Russian: Прогресс M-32) was a Russian unmanned Progress cargo spacecraft, which was launched in July 1996 to resupply the Mir space station.
Progress M-32 launched on 31 July 1996 from the Baikonur Cosmodrome in Kazakhstan. It used a Soyuz-U rocket. [2] [4] The launch was postponed several times, primarily following problems with quality control during Soyuz-U production. [5]
Progress M-32 docked with the forward port of the Mir Core Module on 2 August 1996 at 22:03:40 UTC, and was undocked on 18 August 1996 at 09:33:45 UTC to make way for Soyuz TM-24. [5] [3] On 3 September 1996 at 09:35:00 UTC, Progress M-32 was redocked at the aft port of the Kvant-1 module of Mir, following the departure of Soyuz TM-23. Progress M-32 was finally undocked on 20 November 1996 at 19:51:20 UTC. [5] [3]
It remained in orbit until 20 November 1996, when it was deorbited. The deorbit burn occurred at 22:42:25 UTC. [5] [3]