YF-22A/23A
Engine · China
Original archive entry. The text, images and links below are kept as they were written.
Beijing Wan Yuan N2O4/UDMH rocket engine. Out of production. Cluster of YF-22A and 4 x YF-23 verniers. Boosted CZ-2C, CZ-3. First flight 1975.
Thrust (sl): 697.400 kN (156,782 lbf). Thrust (sl): 71,115 kgf. Chamber Pressure: 71.00 bar. Area Ratio: 10.
Related
- Family
- Storable liquid
- Country
- China
- Launch Vehicles
- Chang Zheng 2C, Chang Zheng 3
- Propellants
- N2O4/UDMH
- Stages
- CZ-2C/SD-2, CZ-2C-2, CZ-3-2
- Agency
- Beijing Wan Yuan