M-13

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Model: Mu-3S-1. Gross Mass: 34,800 kg (76,700 lb). Empty Mass: 7,640 kg (16,840 lb). Thrust (vac): 1,262.419 kN (283,803 lbf). Isp: 263 sec. Burn time: 70 sec. Propellants: Solid. Isp(sl): 238 sec. Diameter: 1.41 m (4.62 ft). Span: 5.00 m (16.40 ft). Length: 14.75 m (48.39 ft). Country: Japan. No Engines: 1. Motor: M-13. Status: Retired 1995. Cost $ : 0.430 million. First Flight: 1977. Last Flight: 1995. No Launched: 12. Other designations: M-13. Model: M-13TVC. Gross Mass: 34,200 kg (75,300 lb). Empty Mass: 6,987 kg (15,403 lb). Thrust (vac): 1,020.000 kN (229,300 lbf). Burn time: 66 sec. Propellants: Solid. Diameter: 1.41 m (4.62 ft). Length: 14.80 m (48.50 ft). Country: Japan. No Engines: 1. Motor: M-13. Status: Retired 1984. First Flight: 1980. Last Flight: 1984. No Launched: 4. 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.