YF-3
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-1D launch vehicle. First flight 1995.
Thrust (sl): 266.300 kN (59,867 lbf). Thrust (sl): 27,160 kgf. Thrust to Weight Ratio: 0.
Related
- Family
- Storable liquid
- Country
- China
- Launch Vehicles
- Chang Zheng 1D
- Propellants
- N2O4/UDMH
- Stages
- CZ-1D-2
- Agency
- Beijing Wan Yuan