M-30

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Model: Mu-3D-3. Gross Mass: 2,800 kg (6,100 lb). Empty Mass: 773 kg (1,704 lb). Thrust (vac): 128.000 kN (28,775 lbf). Burn time: 42 sec. Propellants: Solid. Diameter: 0.86 m (2.82 ft). Length: 4.00 m (13.10 ft). Country: Japan. No Engines: 1. Motor: M-30. Status: Retired 1972. First Flight: 1966. Last Flight: 1972. No Launched: 6. Used as: M-30. 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.