Function: | Carrier rocket | ||||||||||||||||||||||||||||||||||||||
Manufacturer: | CALT | ||||||||||||||||||||||||||||||||||||||
Country-Origin: | China | ||||||||||||||||||||||||||||||||||||||
Status: | Active | ||||||||||||||||||||||||||||||||||||||
Sites: | LA-2 & LA-3, XSLC | ||||||||||||||||||||||||||||||||||||||
Height: | 52.52m (172.31feet)[1] | ||||||||||||||||||||||||||||||||||||||
Diameter: | 3.35m (10.99feet) | ||||||||||||||||||||||||||||||||||||||
Mass: | 241000kg (531,000lb) | ||||||||||||||||||||||||||||||||||||||
Stages: | 3 | ||||||||||||||||||||||||||||||||||||||
Launches: | 27 | ||||||||||||||||||||||||||||||||||||||
Success: | 27 | ||||||||||||||||||||||||||||||||||||||
First: | 8 February 1994 | ||||||||||||||||||||||||||||||||||||||
Capacities: |
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Family: | Long March | ||||||||||||||||||||||||||||||||||||||
Derivatives: | Long March 3B Long March 3C | ||||||||||||||||||||||||||||||||||||||
Stagedata: |
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Last: | 9 July 2018 |
The Long March 3A, also known as the Chang Zheng 3A, CZ-3A and LM-3A, is a Chinese orbital carrier rocket design. It is a 3-stage rocket, and is usually used to place communications satellites and Beidou navigation satellites into geosynchronous transfer orbits.
It has formed the basis of the Long March 3B, which is a heavier version with four liquid booster rockets.
Long March 3A rockets have been launched from Launch Areas 2 and 3 at the Xichang Satellite Launch Center.
See main article: List of Long March launches.
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Flight number | Serial number | Date (UTC) | Launch site | Payload | Orbit | Result |
1 | Y1 | February 8, 1994 08:34 | LA-2, XSLC | Shijian 4 | HEO | |
2 | Y2 | November 29, 1994 17:02 | LA-2, XSLC | Dong Fang Hong 3 | GTO | |
3 | Y3 | May 11, 1997 16:17 | LA-2, XSLC | ChinaSat 6 | GTO | |
4 | Y4 | January 25, 2000 16:45 | LA-2, XSLC | ChinaSat 22 | GTO | |
5 | Y5 | October 30, 2000 16:02 | LA-2, XSLC | Beidou-1A | GTO | |
6 | Y6 | December 20, 2000 16:20 | LA-2, XSLC | Beidou-1B | GTO | |
7 | Y7 | May 24, 2003 16:34 | LA-2, XSLC | Beidou-1C | GTO | |
8 | Y8 | November 14, 2003 16:01 | LA-2, XSLC | ChinaSat 20 | GTO | |
9 | Y9 | October 19, 2004 01:20 | LA-2, XSLC | Fengyun 2C | GTO | |
10 | Y10 | September 12, 2006 16:02 | LA-2, XSLC | ChinaSat 22A | GTO | |
11 | Y11 | December 8, 2006 00:53 | LA-2, XSLC | Fengyun 2D | GTO | |
12 | Y12 | February 2, 2007 16:28 | LA-2, XSLC | Beidou-1D | GTO | |
13 | Y13 | April 13, 2007 20:11 | LA-3, XSLC | Compass-M1 | MEO | |
14 | Y15 | May 31, 2007 16:08 | LA-3, XSLC | SinoSat 3 | GTO | |
15 | Y14 | October 24, 2007 10:05 | LA-3, XSLC | Chang'e 1 | LTO | |
16 | Y20 | December 23, 2008 00:54 | LA-3, XSLC | Fengyun 2E | GTO | |
17 | Y16 | July 31, 2010 21:30 | LA-3, XSLC | Compass-IGSO1 | GTO | |
18 | Y21 | November 24, 2010 16:09 | LA-3, XSLC | ChinaSat 20A | GTO | |
19 | Y18 | December 17, 2010 20:20 | LA-3, XSLC | Compass-IGSO2 | GTO | |
20 | Y19 | April 9, 2011 20:47 | LA-3, XSLC | Compass-IGSO3 | GTO | |
21 | Y17 | July 26, 2011 21:44 | LA-3, XSLC | Compass-IGSO4 | GTO | |
22 | Y23 | December 1, 2011 21:07 | LA-3, XSLC | Compass-IGSO5 | GTO | |
23 | Y22 | January 13, 2012 00:56 | LA-3, XSLC | Fengyun 2F | GTO | |
24 | Y24 | December 31, 2014 01:02 | LA-2, XSLC | Fengyun 2G | GTO | |
25 | Y26 | March 29, 2016 20:11 | LA-2, XSLC | Compass-IGSO6 | GTO | |
26 | Y25 | June 5, 2018 13:07 | LA-2, XSLC | Fengyun 2H | GTO | |
27 | Y27 | July 9, 2018 20:58 | LA-2, XSLC | Compass-IGSO7 | GTO | |
LM-3A is a 3-stage launch vehicle developed on the basis of LM-3 and LM-2C. Its third stage is powered by cryogenic propellants: liquid hydrogen and liquid oxygen. It is dedicated for launching spacecraft into GTO. Its launch capability for GTO mission is 2,600 kg. The fairing static envelope is 3m in diameter.