Encyclopedia entry

Vexin A

Engine · France

Original archive entry. The text, images and links below are kept as they were written.

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

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.