This page no longer updated from 31 October 2001. Latest version can be found at ESEX Arcjet

Designer: Rocket Research. Propellants: Electric/Ammonia Thrust(vac): 0 kgf. Thrust(vac): 0.00 kN. Isp: 800 sec. Chambers: 1. Country: USA. Status: In Production. Comments: Fuel: ammonia at 0.25mg/sec steady state. Design Life: 1500 hours and 400 on/off cycles.
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Last update 12 March 2001.
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© Mark Wade, 2001 .