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CZ-3A
CZ-3A -

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Family: Long March. Country: China. Status: Hardware. Other Designations: Long March 3A.

The Long March 3A was a three-stage launch vehicle. By incorporating the mature technologies of the CZ-3 and adding a more powerful cryogenic third stage and more capable control system, the CZ-3A had a greater geosynchronous transfer orbit capability, greater flexibility for attitude control, and better adaptability to a variety of launch missions. The CZ-3A's geosynchronous transfer orbit payload capability was 2,700kg. By June 30, 1998, the CZ-3A had made three consecutive successful launches, and was offered to international customers.


Specifications

Launches: 4. Failures: 0. Success Rate: 100.00% pct. First Launch Date: 08 February 1994. Last Launch Date: 25 January 2000. LEO Payload: 7,200 kg. to: 200 km Orbit. at: 28.5 degrees. Payload: 2,600 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 302,000 kgf. Total Mass: 241,000 kg. Core Diameter: 3.4 m. Total Length: 52.5 m. Launch Price $: 55.00 million. in 1999 price dollars.


CZ-3A Chronology


1994 Feb 8 - - 08:30 GMT. LV Configuration: Chang Zheng 3A s/n CZ3A-1. Launch Site: Xichang . Launch Complex: LC2.
1994 Nov 29 - - 17:02 GMT. LV Configuration: Chang Zheng 3A s/n CZ3A-2. Launch Site: Xichang . Launch Complex: LC2.
1997 May 11 - - 16:17 GMT. LV Configuration: Chang Zheng 3A s/n CZ3A-3. Launch Site: Xichang . Launch Complex: .
2000 Jan 25 - - 16:45 GMT. LV Configuration: CZ-3A s/n CZ3A-4. Launch Site: Xichang . Launch Complex: LC2.

Bibliography:



LM-3ALM-3A - Long March LM-3A launch vehicle on the launch pad.

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