M-20

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Model: M-20. Gross Mass: 9,900 kg (21,800 lb). Empty Mass: 2,779 kg (6,126 lb). Thrust (vac): 285.000 kN (64,070 lbf). Burn time: 66 sec. Propellants: Solid. Diameter: 1.41 m (4.62 ft). Length: 4.70 m (15.40 ft). Country: Japan. No Engines: 1. Motor: M-20. Status: Retired 1972. First Flight: 1966. Last Flight: 1972. No Launched: 6. Used as: M-20. Release conditions: Nissan. Model: M-22. Gross Mass: 9,800 kg (21,600 lb). Empty Mass: 2,607 kg (5,747 lb). Thrust (vac): 285.000 kN (64,070 lbf). Burn time: 66 sec. Propellants: Solid. Diameter: 1.41 m (4.62 ft). Length: 5.00 m (16.40 ft). Country: Japan. No Engines: 1. Motor: M-22. Status: Retired 1984. First Flight: 1974. Last Flight: 1984. No Launched: 11. No Failed: 1. Used as: M-20. Release conditions: Nissan. Used on Launch Vehicles: Mu. 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.