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CZ-1C-3 engine
Part of CZ-1C-3 Family
Chinese N2O4/UDMH rocket engine. Development ended 1988. Used on CZ-1C launch vehicle.

AKA: CZ-1C-3. Status: Development ended 1988. Thrust: 107.90 kN (24,257 lbf). Specific impulse: 287 s. Specific impulse sea level: 258 s. Burn time: 164 s. Diameter: 1.80 m (5.90 ft).

Thrust (sl): 97.000 kN (21,806 lbf). Thrust (sl): 9,889 kgf.



Family: Storable liquid. Country: China. Launch Vehicles: Chang Zheng 1C. Propellants: N2O4/UDMH. Stages: CZ-1C-3.

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