This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Mitsubishi. Used on stages: LACE. Used on launch vehicles: H-2 HIMES. Propellants: Liquid Air/LH2 Thrust(vac): 15,000 kgf. Thrust(vac): 147.10 kN. Isp: 1,200 sec. Isp (sea level): 600 sec. Burn time: 470 sec. Diameter: 2.4 m. Chambers: 1. Country: Japan. Status: Design concept 1991.
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Last update 12 March 2001.
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© Mark Wade, 2001 .