Long March 3A Explained

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:
Location:LEO
Kilos:8500kg (18,700lb)[2] [3]
Location:GTO
Kilos:2600kg (5,700lb)[4]
Location:HCO
Kilos:1600kg (3,500lb)
Family:Long March
Derivatives:Long March 3B
Long March 3C
Stagedata:
Type:stage
Stageno:First
Length:23.272 m
Diameter:3.35 m
Propmass:171800kg (378,800lb)
Thrust:2961.6kN
Burntime:148 s
Si:2556.5m/s
Type:stage
Stageno:Second
Length:11.276 m
Diameter:3.35 m
Propmass:32600kg (71,900lb)
Engines:1 YF-24E
(1 x YF-22E (Main))
(4 x YF-23C (Vernier))
Thrust:742kN (Main)
47.1kN (Vernier)
Burntime:115 s
Si:2922.57m/s (Main)
2910.5m/s (Vernier)
Type:stage
Stageno:Third
Length:12.375 m
Diameter:3.0 m
Propmass:18200kg (40,100lb)
Engines:2 YF-75[5]
Thrust:167.17kN
Burntime:475 s
Si:4295m/s
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.

Launches

Long March 3A rockets have been launched from Launch Areas 2 and 3 at the Xichang Satellite Launch Center.

List of launches

See main article: List of Long March launches.

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Flight numberSerial numberDate (UTC)Launch sitePayloadOrbitResult
1Y1February 8, 1994
08:34
LA-2, XSLCShijian 4HEO
2Y2November 29, 1994
17:02
LA-2, XSLCDong Fang Hong 3GTO
3Y3May 11, 1997
16:17
LA-2, XSLCChinaSat 6GTO
4Y4January 25, 2000
16:45
LA-2, XSLCChinaSat 22GTO
5Y5October 30, 2000
16:02
LA-2, XSLCBeidou-1AGTO
6Y6December 20, 2000
16:20
LA-2, XSLCBeidou-1BGTO
7Y7May 24, 2003
16:34
LA-2, XSLCBeidou-1CGTO
8Y8November 14, 2003
16:01
LA-2, XSLCChinaSat 20GTO
9Y9October 19, 2004
01:20
LA-2, XSLCFengyun 2CGTO
10Y10September 12, 2006
16:02
LA-2, XSLCChinaSat 22AGTO
11Y11December 8, 2006
00:53
LA-2, XSLCFengyun 2DGTO
12Y12February 2, 2007
16:28
LA-2, XSLCBeidou-1DGTO
13Y13April 13, 2007
20:11
LA-3, XSLCCompass-M1MEO
14Y15May 31, 2007
16:08
LA-3, XSLCSinoSat 3GTO
15Y14October 24, 2007
10:05
LA-3, XSLCChang'e 1LTO
16Y20December 23, 2008
00:54
LA-3, XSLCFengyun 2EGTO
17Y16July 31, 2010
21:30
LA-3, XSLCCompass-IGSO1GTO
18Y21November 24, 2010
16:09
LA-3, XSLCChinaSat 20AGTO
19Y18December 17, 2010
20:20
LA-3, XSLCCompass-IGSO2GTO
20Y19April 9, 2011
20:47
LA-3, XSLCCompass-IGSO3GTO
21Y17July 26, 2011
21:44
LA-3, XSLCCompass-IGSO4GTO
22Y23December 1, 2011
21:07
LA-3, XSLCCompass-IGSO5GTO
23Y22January 13, 2012
00:56
LA-3, XSLCFengyun 2FGTO
24Y24December 31, 2014
01:02
LA-2, XSLCFengyun 2GGTO
25Y26March 29, 2016
20:11
LA-2, XSLCCompass-IGSO6GTO
26Y25June 5, 2018
13:07
LA-2, XSLCFengyun 2HGTO
27Y27July 9, 2018
20:58
LA-2, XSLCCompass-IGSO7GTO

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.

Notes and References

  1. Web site: CZ-3A . Mark Wade . . 2010-05-25 . dead . https://web.archive.org/web/20090611001414/http://www.astronautix.com/lvs/cz.htm . 2009-06-11 .
  2. Web site: LM-3A Series Launch Vehicle User's Manual - Issue 2011. China Great Wall Industries Corporation. 2015-08-09. 2016-12-20. https://web.archive.org/web/20161220124025/http://www.cgwic.com/LaunchServices/Download/manual/LM-3A%20Series%20Launch%20Vehicles%20User%27s%20Manual%20Issue%202011.pdf. dead.
  3. Web site: CZ-3A (Chang Zheng-3A). Gunter Krebs. Gunter's Space Page. 2008-04-27.
  4. Web site: LM-3A. China Great Wall Industry Corporation. 2010-05-25.
  5. Web site: Long March 3C/E - Rockets. Spaceflight101.com. 2016-11-25.