M-3A

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Model: M-3A. Gross Mass: 1,100 kg (2,400 lb). Empty Mass: 130 kg (280 lb). Thrust (vac): 61.000 kN (13,713 lbf). Burn time: 54 sec. Propellants: Solid. Diameter: 1.14 m (3.74 ft). Length: 2.30 m (7.50 ft). Country: Japan. No Engines: 1. Motor: M-3A. Status: Retired 1984. First Flight: 1974. Last Flight: 1984. No Launched: 11. Used as: M-40. 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.