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astronautix.com Vexin C


Designer: SEP. Used on stages: Diamant B-1. Used on launch vehicles: Diamant B. Propellants: N2O4/UDMH Thrust(vac): 10,108 kgf. Thrust(vac): 99.10 kN. Isp: 251 sec. Isp (sea level): 221 sec. Burn time: 110 sec. Mass Engine: 252 kg. Diameter: 0.4 m. Chambers: 1. Thrust to Weight Ratio: 40.11. Country: France. Status: Out of Production. First Flight: 1970. Last Flight: 1975. Flown: 36.
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Last update 12 March 2001.
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