This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Mitsubishi. Used on stages: HIMES. Used on launch vehicles: H-2 HIMES. Propellants: Lox/LH2 Thrust(vac): 14,000 kgf. Thrust(vac): 137.30 kN. Isp: 452 sec. Isp (sea level): 340 sec. Burn time: 167 sec. Chambers: 1. Country: Japan. Status: Study -1998.
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Last update 12 March 2001.
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© Mark Wade, 2001 .