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Chang Zheng 1C
Part of DF-3
Chinese orbital launch vehicle. Proposed launch vehicle derived from the CZ-1, with a new upper stage. Never flown.

AKA: Chang Zheng-1C;CZ-1C;Long March 1C. Status: Development ended 1988. Payload: 500 kg (1,100 lb). Thrust: 1,101.20 kN (247,560 lbf). Gross mass: 85,950 kg (189,480 lb). Height: 33.00 m (108.00 ft). Diameter: 2.25 m (7.38 ft). Apogee: 330 km (200 mi).

LEO Payload: 500 kg (1,100 lb) to a 330 km orbit.

Stage Data - CZ-1C



Family: orbital launch vehicle. Country: China. Engines: CZ-1C-3 engine, YF-2A. Stages: CZ-1C-3, CZ-1-2, CZ-YF-2. Agency: CALT.

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