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CZ-1C-3
N2O4/UDMH propellant rocket stage. .

AKA: CZ-1-3. Status: Development ended 1988. Thrust: 107.00 kN (24,054 lbf). Gross mass: 6,400 kg (14,100 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 287 s. Specific impulse sea level: 258 s. Burn time: 164 s. Height: 4.50 m (14.70 ft). Diameter: 1.80 m (5.90 ft). Span: 1.80 m (5.90 ft).

Cost $ : 0.600 million.



Subtopics

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

Country: China. Engines: CZ-1C-3 engine. Launch Vehicles: Chang Zheng 1C. Propellants: N2O4/UDMH.

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