YF-40
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. Used on CZ-4A launch vehicle. First flight 1988.
Thrust (sl): 43.200 kN (9,712 lbf). Thrust (sl): 4,407 kgf. Thrust to Weight Ratio: 0.
Related
- Family
- Storable liquid
- Country
- China
- Launch Vehicles
- Chang Zheng 4
- Propellants
- N2O4/UDMH
- Agency
- Beijing Wan Yuan