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Mars-Grunt, also known as Expedition-M (Russian: Марс-Грунт), is a proposed robotic Mars sample-return mission. It was proposed to the Russian Federal Space Agency (Roscosmos) by the Russian Space Research Institute.
Cruise stage, Lander & Status
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mars russian roscosmos lander proposed orbiter npo lavochkin mission space agency research institute fobos-grunt sample-return also fobos-grunt-2 expedition-m federal would
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Mars-Grunt | Apo altitude | 500 km (310 mi) | 1.00 | infobox |
| Mars-Grunt | Bus | Pereletny Modul or Flagman | 1.00 | infobox |
| Mars-Grunt | Contractor | Roscosmos | 1.00 | infobox |
| Mars-Grunt | Dry mass | Orbiter: 450 kg (990 lb) | 1.00 | infobox |
| Mars-Grunt | Landing mass | 2,750 kg, including Mars Ascent Vehicle (450 kg) | 1.00 | infobox |
| Mars-Grunt | Launch date | 2030s (proposed) | 1.00 | infobox |
| Mars-Grunt | Launch mass | 4,100 kg | 1.00 | infobox |
| Mars-Grunt | Launch site | Vostochny Site 1A | 1.00 | infobox |
| Mars-Grunt | Manufacturer | NPO Lavochkin Russian Space Research Institute | 1.00 | infobox |
| Mars-Grunt | Mission type | Single launch: orbiter, lander, ascent vehicle, sample-return | 1.00 | infobox |
| Mars-Grunt | Names | Expedition-M | 1.00 | infobox |
| Mars-Grunt | Operator | Russian Federal Space Agency | 1.00 | infobox |
| Mars-Grunt | Peri altitude | 500 km (310 mi) | 1.00 | infobox |
| Mars-Grunt | Power | solar array | 1.00 | infobox |
| Mars-Grunt | Rocket | Angara A5 / KTVK | 1.00 | infobox |
| Mars-Grunt | Sample mass | ≈0.2 kg (0.44 lb) | 1.00 | infobox |
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