YF-22/23
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-22 and 4 x YF-23 verniers. Boosted CZ-2A, FB-1. First flight 1972.
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
- Feng Bao 1, Chang Zheng 2
- Propellants
- N2O4/UDMH
- Stages
- FB-1-2
- Agency
- Beijing Wan Yuan