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CZ-1-2
Nitric acid/UDMH propellant rocket stage. Masses, engine performance estimated based on successor improved stage and YF-2 engines in first stage.

Status: Retired 1971. Thrust: 306.14 kN (68,824 lbf). Gross mass: 15,000 kg (33,000 lb). Unfuelled mass: 2,700 kg (5,900 lb). Specific impulse: 275 s. Specific impulse sea level: 200 s. Burn time: 110 s. Height: 5.35 m (17.55 ft). Diameter: 2.25 m (7.38 ft). Span: 2.25 m (7.38 ft).

Cost $ : 1.000 million.



Subtopics

CZ-1D-2 N2O4/UDMH propellant rocket stage. .

Country: China. Engines: YF-2A. Launch Vehicles: DF-4, Chang Zheng 1, Chang Zheng 1M, Chang Zheng 1C. Propellants: Nitric acid/UDMH.

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