This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Aerojet. Propellants: N2O4/MMH Thrust(vac): 2 kgf. Thrust(vac): 0.02 kN. Isp: 285 sec. Mass Engine: 1 kg. Chambers: 1. Area Ratio: 75.00. Country: USA. Status: In Production. Comments: Mixture Ratio(O/F): 1.60.
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Last update 12 March 2001.
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© Mark Wade, 2001 .