Viking 2B
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 2/3. First flight 1984.
Thrust (sl): 642.300 kN (144,395 lbf). Thrust (sl): 65,496 kgf. Engine: 776 kg (1,710 lb). Chamber Pressure: 59.00 bar. Area Ratio: 11. Thrust to Weight Ratio: 86.3758823529412.
Related
- Family
- Storable liquid
- Country
- France
- Launch Vehicles
- Ariane 2/3, Ariane 4, Ariane 44LP, Ariane 44L, Ariane 42P, Ariane 44P, Ariane 42L
- Propellants
- N2O4/UDMH
- Stages
- Ariane 2-1, Ariane 4-1