This page no longer updated from 31 October 2001. Latest version can be found at M-23-Mu

Designer: Nissan. Used on stages: Mu-3S-2. Used on launch vehicles: Mu-3S. Gross Mass: 13,100 kg. Empty Mass: 2,800 kg. Propellants: Solid Thrust(vac): 53,433 kgf. Thrust(vac): 524.00 kN. Isp: 285 sec. Isp (sea level): 220 sec. Burn time: 70 sec. Diameter: 1.4 m. Length: 6.2 m. Chambers: 1. Country: Japan. Status: In Production. First Flight: 1970. Last Flight: 1995. Flown: 23.
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Last update 12 March 2001.
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© Mark Wade, 2001 .