This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Liberty 2. Used on launch vehicles: Liberty. Propellants: N2O4/MMH Thrust(vac): 1,814 kgf. Thrust(vac): 17.80 kN. Isp: 300 sec. Isp (sea level): 200 sec. Burn time: 326 sec. Mass Engine: 41 kg. Diameter: 1.4 m. Chambers: 1. Area Ratio: 98.00. Country: USA. Status: Developed 1982-1988. Comments: Pressure-fed engine.
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Last update 12 March 2001.
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© Mark Wade, 2001 .