This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Europa-3. Used on launch vehicles: Europa. Propellants: N2O4/Aerozine-50 Thrust(vac): 2,380 kgf. Thrust(vac): 23.30 kN. Isp: 310 sec. Isp (sea level): 260 sec. Burn time: 330 sec. Mass Engine: 68 kg. Diameter: 2.0 m. Chambers: 1. Thrust to Weight Ratio: 35.00. Country: Germany. Status: Out of Production. First Flight: 1964. Last Flight: 1971. Flown: 11.
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Last update 12 March 2001.
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© Mark Wade, 2001 .