CZ-1C-3 engine
Engine · China
Original archive entry. The text, images and links below are kept as they were written.
Chinese N2O4/UDMH rocket engine. Development ended 1988. Used on CZ-1C launch vehicle.
Thrust (sl): 97.000 kN (21,806 lbf). Thrust (sl): 9,889 kgf.
Related
- Family
- Storable liquid
- Country
- China
- Launch Vehicles
- Chang Zheng 1C
- Propellants
- N2O4/UDMH
- Stages
- CZ-1C-3