Vexin C

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Vexin C

Part of Vexin A

SEP N2O4/UDMH rocket engine. Out of production. Used on Diamant B launch vehicle. First flight 1970.

Status: Out of production. Number: 20 . Thrust: 99.10 kN (22,279 lbf). Unfuelled mass: 252 kg (555 lb). Specific impulse: 251 s. Specific impulse sea level: 221 s. Burn time: 110 s. Diameter: 0.35 m (1.14 ft).

Thrust (sl): 87.300 kN (19,626 lbf). Thrust (sl): 8,900 kgf. Engine: 252 kg (555 lb). Thrust to Weight Ratio: 40.1111111111111.

Family: Storable liquid. Country: France. Launch Vehicles: Diamant B. Propellants: N2O4/UDMH. Stages: Diamant B-1.

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