Vexin C
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 B launch vehicle. First flight 1970.
Thrust (sl): 87.300 kN (19,626 lbf). Thrust (sl): 8,900 kgf. Engine: 252 kg (555 lb). Thrust to Weight Ratio: 40.1111111111111.
Related
- Family
- Storable liquid
- Country
- France
- Launch Vehicles
- Diamant B
- Propellants
- N2O4/UDMH
- Stages
- Diamant B-1