This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Nissan. Used on stages: H-1-3. Used on launch vehicles: H-1. Propellants: Solid Thrust(vac): 7,900 kgf. Thrust(vac): 77.00 kN. Isp: 291 sec. Isp (sea level): 220 sec. Burn time: 68 sec. Diameter: 1.3 m. Length: 2.3 m. Chambers: 1. Country: Japan. Status: Out of Production. First Flight: 1986. Last Flight: 1992. Flown: 9.
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Last update 12 March 2001.
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© Mark Wade, 2001 .