Long March 3A
From Wikipedia, the free encyclopedia
Long March 3A | |
Long March 3A |
|
Fact sheet | |
---|---|
Function | Carrier rocket |
Manufacturer | CALT |
Country of origin | People's Republic of China |
Size | |
Height | 52.5 metres (172 ft)[1] |
Diameter | 3.35 metres (11.0 ft)[1] |
Mass | 241,000 kilograms (530,000 lb)[1] |
Stages | 3 |
Capacity | |
Payload to LEO |
8,500 kilograms (19,000 lb)[2] |
Payload to GTO |
2,300 kilograms (5,100 lb)[2] |
Payload to HCO |
1,600 kilograms (3,500 lb)[2] |
Associated Rockets | |
Family | Long March |
Derivatives | Long March 3B |
Launch History | |
Status | Active |
Launch sites | LC-2, XSLC |
Total launches | 14 |
Successes | 14 |
Maiden flight | 8 February 1994 |
The Long March 3A, also known as the Chang Zheng 3A, CZ-3A and LM-3A, is a Chinese orbital carrier rocket. It is launched from Launch Complex 2 at the Xichang Satellite Launch Centre. It is a 3-stage rocket, and is ususally used to place communications satellites and Beidou navigation satellites into geosynchronous transfer orbits. It first flew on 8 February 1994. On 24 October 2007, a Long March 3A launched Chang'e-1, the first Chinese Lunar probe.
It has formed the basis of the Long March 3B, which is a heavier version with four liquid booster rockets. This first flew in 1996.
[edit] References
|
|