Viking 5C
Engine · France
Original archive entry. The text, images and links below are kept as they were written.
SEP N2O4/UDMH rocket engine. Used on Ariane 42L, Ariane 44L, Ariane 44LP. First flight 1988.
Thrust (sl): 670.800 kN (150,802 lbf). Thrust (sl): 68,408 kgf. Engine: 776 kg (1,710 lb). Chamber Pressure: 55.00 bar. Area Ratio: 11. Thrust to Weight Ratio: 92.8361491718405. Oxidizer to Fuel Ratio: 1.7. Coefficient of Thrust vacuum: 1.74615169837655. Coefficient of Thrust sea level: 1.56511721561793.
Related
- Family
- Storable liquid
- Country
- France
- Launch Vehicles
- Ariane 44LP, Ariane 44L, Ariane 42L
- Propellants
- N2O4/UDMH
- Stages
- Ariane 4-0-4L
- Bibliography
- 225