YF-2A
Engine · China
Original archive entry. The text, images and links below are kept as they were written.
Beijing Wan Yuan Nitric acid/UDMH rocket engine. Out of production. Used on CZ-1, CZ-1C, CZ-1D, CZ-1M. First flight 1969.
Thrust (sl): 275.300 kN (61,890 lbf). Thrust (sl): 28,073 kgf. Chamber Pressure: 71.00 bar. Area Ratio: 10. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 1.50569884121406. Coefficient of Thrust sea level: 1.36485377079152.
Related
- Family
- Storable liquid
- Country
- China
- Launch Vehicles
- Chang Zheng 1, Chang Zheng 1M, Chang Zheng 1C, Chang Zheng 1D
- Propellants
- Nitric acid/UDMH
- Agency
- Beijing Wan Yuan