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CZ-2D
CZ-2D -

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Family: Long March. Country: China. Status: Hardware. Other Designations: Long March 2D.

The Long March 2D was a two-stage launch vehicle with storable propellants, suitable for launching a variety of low earth orbit satellites. Developed and manufactured by the Shanghai Academy of Spaceflight Technology, the CZ-2D had a typical payload capability of 3,500kg in a 200 km circular orbit. Its first stage was identical to that of the CZ-4. The second stage was essentially the same as that of the CZ-4, except for an improved vehicle equipment bay.


Specifications

Launches: 3. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 09 August 1992. Last Launch Date: 20 October 1996. LEO Payload: 3,500 kg. to: 200 km Orbit. at: 28.0 degrees. Liftoff Thrust: 298,389 kgf. Total Mass: 232,250 kg. Core Diameter: 3.4 m. Total Length: 35.1 m. Launch Price $: 15.00 million. in 1999 price dollars.


CZ-2D Chronology


1992 Aug 9 - - 07:55 GMT. LV Configuration: Chang Zheng 2D s/n CZ2D-1. Launch Site: Jiuquan . Launch Complex: LA2.
1994 Jul 3 - - 08:00 GMT. LV Configuration: Chang Zheng 2D s/n CZ2D-2. Launch Site: Jiuquan . Launch Complex: LA2.
1996 Oct 20 - - 07:20 GMT. LV Configuration: Chang Zheng 2D s/n CZ2D-3.

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