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Chang Zheng 1D
Part of DF-3

Chinese solids

Chinese solids

Chinese orbital launch vehicle. Proposed launch vehicle derived from the CZ-1, but with a new N2O4/UDMH second stage. Used for a suborbital re-entry vehicle test but never flown on an orbital mission.

AKA: Chang Zheng-1D;CZ-1D;Long March 1D. Status: Retired 1997. First Launch: 1995-05-29. Last Launch: 1997-11-01. Number: 2 . Payload: 740 kg (1,630 lb). Thrust: 1,101.20 kN (247,560 lbf). Gross mass: 79,400 kg (175,000 lb). Height: 28.22 m (92.58 ft). Diameter: 2.25 m (7.38 ft). Apogee: 300 km (180 mi).

LEO Payload: 740 kg (1,630 lb) to a 300 km orbit. Payload: 440 kg (970 lb) to a GTO. Launch Price $: 12.000 million in 1994 dollars.

Stage Data - CZ-1D



Family: orbital launch vehicle. Country: China. Engines: YF-3, YF-2A. Launch Sites: Taiyuan. Stages: CZ-YF-2, CZ-1D-2, CZ-1D-3, GF-02. Agency: CALT.

1995 May 29 - . Launch Site: Taiyuan. LV Family: DF-3. Launch Vehicle: Chang Zheng 1D.
1997 November 1 - . Launch Site: Taiyuan. LV Family: DF-3. Launch Vehicle: Chang Zheng 1D.

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