M-10

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Model: Mu-4S-1. Gross Mass: 26,600 kg (58,600 lb). Empty Mass: 5,907 kg (13,022 lb). Thrust (vac): 737.000 kN (165,684 lbf). Burn time: 61 sec. Propellants: Solid. Diameter: 1.41 m (4.62 ft). Length: 13.00 m (42.00 ft). Country: Japan. No Engines: 1. Motor: M-10. Status: Retired 1979. First Flight: 1966. Last Flight: 1979. No Launched: 12. Used as: Mu. 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.