Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.


Fobos-Grunt [Lavochkin]

Fobos-Grunt (Cruise configuration) [Lavochkin]

The Russian Fobos-Grunt mission's objectives were to collect soil samples from Phobos, a satellite of Mars and to bring the samples back to Earth for comprehensive scientific research into Phobos, Mars and Martian space.

Studies were to include:

  • both in situ and remote studies of Phobos, including laboratory analysis of the soil samples
  • monitoring the planet Mars, including the holistic dynamic behaviour of the atmosphere and dust storms
  • studies of Martian surroundings, including plasma and dust components, and the radiation environment

The space mission component development was led by the company NPO Lavochkin. Phobos soil sampling and downloading had been assigned to the GEOHI RAN Institute of the Russian Academy of Science (Vernadski Institute of Geochemistry and Analytical chemistry) and the integrated scientific studies of Phobos and Mars by remote and contact methods were developed by the IKI RAN Institute (Space Research Institute).

In 2007 the chinese space agency signed an agreement to launch the 110 kg Yinghuo 1 orbiter piggyback on Fobos-Grunt. This orbiter was to separate from Fobos-Grunt after reaching mars orbit. Originally planned was also the Russian-finnish small Mars Meteorological Station (MMS), which was cancelled later.

A propulsion module called MDU based on an modified Fregat-SB upper stage was also to act as the cruise stage. It was to remain attached to Fobos Grunt by a truss adaptor, which contained the Yinghuo 1 probe. After Martian orbit insertion, Fobos Grunt was to separate from the Fregat enabling Yinghuo 1 to be separated.

As the propulsion module provides the trans-Mars-injection, a two stage Zenit-2FG rocket launched Fobos-Grunt into low earth orbit.

After launch, Fobos-Grunt failed to ignite the propulsion module, went into safe-mode and remained in low earth orbit. The mission was lost as the Fobos-Grunt probe could not be commanded in several communication attempts to fire the propulsion module. Fobos-Grunt, Yinghuo 1 and the Fregat propulsion module reentered the earth atmosphere on 15. January 2012.

Nation: Russia
Type / Application: Phobos lander
Contractors: NPO Lavochkin
Propulsion: 3 × SPT-140
Power: 2 deployable fixed solar arrays, batteries
Orbit: Mars orbit
Satellite COSPAR Date LS Launch Vehicle Remarks
Fobos-Grunt 2011-065A 08.11.2011 Ba LC-45/1 P Zenit-2FG [Fregat-SB] with Yinghuo 1

Cite this page: