This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Sea Horse-1. Used on launch vehicles: Sea Horse. Propellants: Lox/Kerosene Thrust(vac): 77,000 kgf. Thrust(vac): 755.10 kN. Isp: 285 sec. Isp (sea level): 250 sec. Burn time: 128 sec. Mass Engine: 643 kg. Diameter: 3.0 m. Chambers: 1. Chamber Pressure: 40.00 bar. Area Ratio: 8.00. Country: USA. Status: Design concept 1982.
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Last update 12 March 2001.
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© Mark Wade, 2001 .