MR-12

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Model: MR-12-1. Gross Mass: 1,000 kg (2,200 lb). Propellants: Solid. Diameter: 0.45 m (1.47 ft). Length: 8.80 m (28.80 ft). Country: Russia. No Engines: 1. Motor: MR-12. Status: Retired 1997. Used as: MR-12. Release conditions: SSSR. Model: MR-25-1. Gross Mass: 1,000 kg (2,200 lb). Propellants: Solid. Diameter: 0.45 m (1.47 ft). Length: 8.80 m (28.80 ft). Country: Russia. No Engines: 1. Motor: MR-25. Status: Retired 1970. First Flight: 1970. Last Flight: 1970. No Launched: 2. Used as: MR-12. Release conditions: SSSR. Model: MR-20-1. Gross Mass: 1,000 kg (2,200 lb). Propellants: Solid. Diameter: 0.45 m (1.47 ft). Length: 8.80 m (28.80 ft). Country: Russia. No Engines: 1. Motor: MR-20. Status: Retired 1991. First Flight: 1979. Last Flight: 1991. No Launched: 109. Used as: MR-12. Release conditions: SSSR. Used on Launch Vehicles: MR-12. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.