Vexin B
Engine · France
Original archive entry. The text, images and links below are kept as they were written.
SEP N2O4/UDMH rocket engine. Out of production. Used on Diamant launch vehicle. First flight 1965.
Thrust (sl): 66.400 kN (14,927 lbf). Thrust (sl): 6,768 kgf. Engine: 192 kg (423 lb). Thrust to Weight Ratio: 40.0364583333333.
Related
- Family
- Storable liquid
- Country
- France
- Launch Vehicles
- Diamant
- Propellants
- N2O4/UDMH
- Stages
- Diamant-1