This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: SEP. Used on stages: Europa-2. Used on launch vehicles: Europa. Propellants: N2O4/UDMH Thrust(vac): 7,000 kgf. Thrust(vac): 68.60 kN. Isp: 277 sec. Isp (sea level): 240 sec. Burn time: 96 sec. Mass Engine: 175 kg. Diameter: 0.5 m. Chambers: 1. Thrust to Weight Ratio: 40.00. Country: France. Status: Out of Production. First Flight: 1964. Last Flight: 1971. Flown: 44.
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Last update 12 March 2001.
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© Mark Wade, 2001 .