Long March 2A
Appearance
Function | Carrier rocket |
---|---|
Manufacturer | CALT |
Country of origin | China |
Size | |
Height | 32 metres (105 ft)[1] |
Diameter | 3.35 metres (11.0 ft)[1] |
Mass | 190,000 kilograms (420,000 lb)[1] |
Stages | 2 |
Capacity | |
Payload to LEO | |
Mass | 2,000 kilograms (4,400 lb)[1] |
Associated rockets | |
Family | Long March |
Derivative work | Long March 2C, 2E, 2F |
Launch history | |
Status | Retired |
Launch sites | LA-2/138, JSLC |
Total launches | 4 |
Success(es) | 3 |
Failure(s) | 1 |
First flight | 5 November 1974 |
Last flight | 26 January 1978 |
The Long March 2A, also known as the Chang Zheng 2A, CZ-2A and LM-2A, was a Chinese orbital carrier rocket.
It was launched from Launch Area 2B at the Jiuquan Satellite Launch Centre. It was a 2-stage rocket, and flew 4 times. On its first flight on 5 November 1974, a cable connecting the pitch rate control gyroscope to the guidance system became disconnected, resulting in a loss of control and launch failure.
The rocket was subsequently replaced by the more capable Long March 2C.
The payloads for the Long March 2A were FSW-0 reconnaissance satellites.
List of launches
Flight number | Date (UTC) | Launch site | Payload | Orbit | Result |
---|---|---|---|---|---|
1 | November 5, 1974 09:40 |
LA-2/138, JSLC | FSW-0 No.0 | LEO | Failure |
2 | November 16, 1975 03:29 |
LA-2/138, JSLC | FSW-0 No.1 | LEO | Success |
3 | December 7, 1976 04:38 |
LA-2/138, JSLC | FSW-0 No.2 | LEO | Success |
4 | January 26, 1978 04:58 |
LA-2/138, JSLC | FSW-0 No.3 | LEO | Success |
References
- ^ a b c d Mark Wade. "CZ-2A". Encyclopedia Astronautica. Archived from the original on 2008-05-16. Retrieved 2008-05-01.