This page no longer updated from 31 October 2001. Latest version can be found at M-3B-Mu

Designer: Nissan. Used on stages: Mu-3S-3. Used on launch vehicles: Mu-3S. Gross Mass: 3,590 kg. Empty Mass: 490 kg. Propellants: Solid Thrust(vac): 13,472 kgf. Thrust(vac): 132.10 kN. Isp: 294 sec. Burn time: 85 sec. Diameter: 1.5 m. Length: 2.7 m. Chambers: 1. Chamber Pressure: 42.00 bar. Area Ratio: 52.00. 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 .