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Vexin A
SEP N2O4/UDMH rocket engine. Used on Europa launch vehicle. First flight 1964.

Number: 44 . Thrust: 68.60 kN (15,422 lbf). Unfuelled mass: 175 kg (385 lb). Specific impulse: 277 s. Specific impulse sea level: 240 s. Burn time: 96 s. Diameter: 0.50 m (1.64 ft).

Thrust (sl): 59.500 kN (13,376 lbf). Thrust (sl): 6,065 kgf. Engine: 175 kg (385 lb). Thrust to Weight Ratio: 40.



Subtopics

Europa-2 N2O4/UDMH propellant rocket stage. .

Diamant B-1 N2O4/UDMH propellant rocket stage. .

Diamant-1 N2O4/UDMH propellant rocket stage. .

Vexin B SEP N2O4/UDMH rocket engine. Out of production. Used on Diamant launch vehicle. First flight 1965.

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

Family: Storable liquid. Country: France. Launch Vehicles: Europa I. Propellants: N2O4/UDMH. Stages: Europa-2.

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