This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Nissan. Used on stages: M-V-1. Used on launch vehicles: M-V. Gross Mass: 83,560 kg. Empty Mass: 12,070 kg. Propellants: Solid Thrust(vac): 385,488 kgf. Thrust(vac): 3,780.30 kN. Isp: 276 sec. Isp (sea level): 246 sec. Burn time: 46 sec. Diameter: 2.5 m. Length: 13.8 m. Chambers: 1. Chamber Pressure: 59.00 bar. Area Ratio: 11.00. Country: Japan. Status: In Production. First Flight: 1997. Last Flight: 1998. Flown: 2.
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Last update 12 March 2001.
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© Mark Wade, 2001 .