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Zenit-2SB
Part of Zenit
Two stage version of the Zenit launch vehicle consisting of 1 x 11S771 + 1 x 11S772.
Status: Active. First Launch: 2011-11-08. Last Launch: 2011-11-08. Number: 1 .
More at: Zenit-2SB.
Country:
Ukraine.
Spacecraft:
Fobos 1F.
Launch Sites:
Baikonur LC45/1.
2011 November 8 - .
20:16 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC45/1.
LV Family:
Zenit.
Launch Vehicle:
Zenit-2SB.
- Fobos-Grunt - .
Mass: 13,500 kg (29,700 lb). Nation: Russia.
Class: Mars.
Type: Mars orbiter. Spacecraft Bus: 5MV.
Spacecraft: Fobos 1F.
Decay Date: 2012-01-15 . USAF Sat Cat: 37872 . COSPAR: 2011-065A. Apogee: 274 km (170 mi). Perigee: 199 km (123 mi). Inclination: 51.40 deg. Period: 89.20 min.
Failed soil-return mission to Martian moon Phobos. The main propulsion system, which was to have boosted the probe out of earth parking orbit to trans-Mars insertion, failed to ignite. Attempts to communicate with the spacecraft partially succeeded but it could not be commanded to conduct an engine burn at a later opportunity. Destroyed on reentry into the earth's atmosphere.
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