Long March 3A
Template:Short description Script error: No such module "For". Script error: No such module "infobox".Script error: No such module "Check for unknown parameters".
The Long March 3A (Template:Zh), 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.
Launches
Long March 3A rockets have been launched from Launch Areas 2 and 3 at the Xichang Satellite Launch Center.
List of launches
Script error: No such module "Labelled list hatnote".
| Flight number | Serial number | Date (UTC) | Launch site | Payload | Orbit | Result |
|---|---|---|---|---|---|---|
| 1 | Y1 | February 8, 1994 08:34 |
LA-2, XSLC | Shijian 4 | HEO | Template:Success |
| 2 | Y2 | November 29, 1994 17:02 |
LA-2, XSLC | Dong Fang Hong 3 | GTO | Template:Success |
| 3 | Y3 | May 11, 1997 16:17 |
LA-2, XSLC | ChinaSat 6 | GTO | Template:Success |
| 4 | Y4 | January 25, 2000 16:45 |
LA-2, XSLC | ChinaSat 22 | GTO | Template:Success |
| 5 | Y5 | October 30, 2000 16:02 |
LA-2, XSLC | Beidou-1A | GTO | Template:Success |
| 6 | Y6 | December 20, 2000 16:20 |
LA-2, XSLC | Beidou-1B | GTO | Template:Success |
| 7 | Y7 | May 24, 2003 16:34 |
LA-2, XSLC | Beidou-1C | GTO | Template:Success |
| 8 | Y8 | November 14, 2003 16:01 |
LA-2, XSLC | ChinaSat 20 | GTO | Template:Success |
| 9 | Y9 | October 19, 2004 01:20 |
LA-2, XSLC | Fengyun 2C | GTO | Template:Success |
| 10 | Y10 | September 12, 2006 16:02 |
LA-2, XSLC | ChinaSat 22A | GTO | Template:Success |
| 11 | Y11 | December 8, 2006 00:53 |
LA-2, XSLC | Fengyun 2D | GTO | Template:Success |
| 12 | Y12 | February 2, 2007 16:28 |
LA-2, XSLC | Beidou-1D | GTO | Template:Success |
| 13 | Y13 | April 13, 2007 20:11 |
LA-3, XSLC | Compass-M1 | MEO | Template:Success |
| 14 | Y15 | May 31, 2007 16:08 |
LA-3, XSLC | SinoSat 3 | GTO | Template:Success |
| 15 | Y14 | October 24, 2007 10:05 |
LA-3, XSLC | Chang'e 1 | LTO | Template:Success |
| 16 | Y20 | December 23, 2008 00:54 |
LA-3, XSLC | Fengyun 2E | GTO | Template:Success |
| 17 | Y16 | July 31, 2010 21:30 |
LA-3, XSLC | Compass-IGSO1 | GTO | Template:Success |
| 18 | Y21 | November 24, 2010 16:09 |
LA-3, XSLC | ChinaSat 20A | GTO | Template:Success |
| 19 | Y18 | December 17, 2010 20:20 |
LA-3, XSLC | Compass-IGSO2 | GTO | Template:Success |
| 20 | Y19 | April 9, 2011 20:47 |
LA-3, XSLC | Compass-IGSO3 | GTO | Template:Success |
| 21 | Y17 | July 26, 2011 21:44 |
LA-3, XSLC | Compass-IGSO4 | GTO | Template:Success |
| 22 | Y23 | December 1, 2011 21:07 |
LA-3, XSLC | Compass-IGSO5 | GTO | Template:Success |
| 23 | Y22 | January 13, 2012 00:56 |
LA-3, XSLC | Fengyun 2F | GTO | Template:Success |
| 24 | Y24 | December 31, 2014 01:02 |
LA-2, XSLC | Fengyun 2G | GTO | Template:Success |
| 25 | Y26 | March 29, 2016 20:11 |
LA-2, XSLC | Compass-IGSO6 | GTO | Template:Success |
| 26 | Y25 | June 5, 2018 13:07 |
LA-2, XSLC | Fengyun 2H | GTO | Template:Success |
| 27 | Y27 | July 9, 2018 20:58 |
LA-2, XSLC | Compass-IGSO7 | GTO | Template:Success |
Technical data
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.[1]
References
Script error: No such module "Portal". Script error: No such module "Navbox". Template:Expendable launch systems Template:CLEP
- ↑ Cite error: Invalid
<ref>tag; no text was provided for refs namedCGWIC