Viking 2
Engine · France
Original archive entry. The text, images and links below are kept as they were written.
SEP N2O4/UDMH rocket engine. In production. Used on Ariane 1, GSLV space launchers. First flight 1979.
Thrust (sl): 611.600 kN (137,493 lbf). Thrust (sl): 62,366 kgf. Engine: 776 kg (1,710 lb). Chamber Pressure: 55.00 bar. Area Ratio: 11. Thrust to Weight Ratio: 91.0631443298969. Coefficient of Thrust vacuum: 1.77769748966301. Coefficient of Thrust sea level: 1.57769748966301.
Subtopics
- Viking 4 SEP N2O4/UDMH rocket engine. Used on Ariane 1, GSLV, PSLV. First flight 1979.
- Viking 2B SEP N2O4/UDMH rocket engine. Used on Ariane 2/3. First flight 1984.
- Viking 4B SEP N2O4/UDMH rocket engine. Used on Ariane 4. First flight 1984.
- Viking 5C SEP N2O4/UDMH rocket engine. Used on Ariane 42L, Ariane 44L, Ariane 44LP. First flight 1988.
Related
- Family
- Storable liquid
- Country
- France
- Propellants
- N2O4/UDMH
- Stages
- Ariane 1-1, GSLV-0