This page no longer updated from 31 October 2001.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-3. Used on launch vehicles: M-V. Gross Mass: 11,000 kg. Empty Mass: 1,000 kg. Propellants: Solid Thrust(vac): 30,000 kgf. Thrust(vac): 294.20 kN. Isp: 301 sec. Burn time: 102 sec. Diameter: 2.2 m. Length: 3.6 m. Chambers: 1. Chamber Pressure: 59.00 bar. Area Ratio: 96.00. 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 .