Long March 4B

The Long March 4B (Chinese: 长征四号乙火箭), also known as the Chang Zheng 4B, CZ-4B and LM-4B is a Chinese orbital carrier rocket. Launched from Launch Complex 1 at the Taiyuan Satellite Launch Center, it is a 3-stage rocket, used mostly to place satellites into low Earth and sun-synchronous orbits. It was first launched on 10 May 1999, with the FY-1C weather satellite, which would later be used in the 2007 Chinese anti-satellite missile test.

Long March 4B
Long March 4B
FunctionCarrier rocket
ManufacturerSAST
Country of originChina
Cost per launchUS$50 million (2006)
Size
Height44.1 metres (145 ft)[1]
Diameter3.35 metres (11.0 ft)[2]
Mass249,200 kilograms (549,400 lb)[2]
Stages3
Capacity
Payload to LEO4,200 kilograms (9,300 lb)[3]
Payload to SSO2,800 kilograms (6,200 lb)[3]
Payload to GTO1,500 kilograms (3,300 lb)[3]
Associated rockets
FamilyLong March
DerivativesLong March 4C
Launch history
StatusActive
Launch sites
Total launches37
Successes36
Failures1
First flight10 May 1999
Last flight25 July 2020
First stage
Length27.91 m
Diameter3.35 m
Propellant mass182,000 kilograms (401,000 lb)
Engines4 YF-21C
Thrust2,961.6 kilonewtons (665,800 lbf)
Specific impulse2,550 metres per second (8,400 ft/s)
FuelN2O4 / UDMH
Second stage
Length10.9 m
Diameter3.35 m
Propellant mass52,700 kilograms (116,200 lb)
Engines1 YF-24C
(1 x YF-22C (Main))
(4 x YF-23C (Vernier))
Thrust742.04 kilonewtons (166,820 lbf) (Main)
47.1 kilonewtons (10,600 lbf) (Vernier)
Specific impulse2,942 metres per second (9,650 ft/s) (Main)
2,834 metres per second (9,300 ft/s) (Vernier)
FuelN2O4 / UDMH
Third stage
Length14.79 m
Diameter2.9 m
Propellant mass14,000 kilograms (31,000 lb)
Engines2 YF-40
Thrust100.85 kilonewtons (22,670 lbf)
Specific impulse2,971 metres per second (9,750 ft/s)
FuelN2O4 / UDMH

The Chang Zheng 4B experienced its only launch failure on 9 December 2013, with the loss of the CBERS-3 satellite.[4]

List of launches

Flight
number
Date and time
(UTC)
Launch site Payload Orbit Result
1 10 May 1999
01:33
Taiyuan
LA-7
Fengyun 1C
Shijian 5
SSO Success
2 14 October 1999
03:15
Taiyuan
LA-7
CBERS-1
SACI-1
SSO Success
3 1 September 2000
03:25
Taiyuan
LA-7
Ziyuan II-01 SSO Success
4 15 May 2002
01:50
Taiyuan
LA-7
Fengyun 1D
HaiYang-1A
SSO Success
5 27 October 2002
03:17
Taiyuan
LA-7
Ziyuan II-02 SSO Success
6 21 October 2003
03:16
Taiyuan
LA-7
CBERS-2
Chuangxin 1-01
SSO Success
7 8 September 2004
23:14
Taiyuan
LA-7
Shijian 6A
Shijian 6B
SSO Success
8 6 November 2004
03:10
Taiyuan
LA-7
Ziyuan II-03 SSO Success
9 23 October 2006
23:34
Taiyuan
LA-7
Shijian 6C
Shijian 6D
SSO Success
10 19 September 2007
03:26
Taiyuan
LA-7
CBERS-2B SSO Success
11 25 October 2008
01:15
Taiyuan
LA-9
Shijian 6E
Shijian 6F
SSO Success
12 15 December 2008
03:22
Taiyuan
LA-9
Yaogan 5 SSO Success
13 6 October 2010
00:49
Taiyuan
LA-9
Shijian 6G
Shijian 6H
SSO Success
14 15 August 2011
22:57
Taiyuan
LA-9
HaiYang-2A SSO Success
15 9 November 2011
03:21
Taiyuan
LA-9
Yaogan 12
Tianxun 1
SSO Success
16 22 December 2011
03:26
Taiyuan
LA-9
Ziyuan I-02C SSO Success
17 9 January 2012
03:17
Taiyuan
LA-9
Ziyuan III-01
VesselSat-2
SSO Success
18 10 May 2012
07:06
Taiyuan
LA-9
Yaogan 14
Tiantuo 1
SSO Success
19 25 October 2013
03:50
Jiuquan
LA-4/SLS-2
Shijian 16-01 LEO Success
20 9 December 2013
03:26
Taiyuan
LA-9
CBERS-3 SSO Failure
One of the two third-stage engines shut down prematurely, so that the satellite failed to reach orbit. The cause was traced to foreign debris that blocked the engine's fuel intake.[5]
21 19 August 2014
03:15
Taiyuan
LA-9
Gaofen 2
BRITE-PL2 (Heweliusz)
SSO Success
22 8 September 2014
03:22
Taiyuan
LA-9
Yaogan 21
Tiantuo 2
SSO Success
23 7 December 2014
03:26
Taiyuan
LA-9
CBERS-4 SSO Success
24 27 December 2014
03:22
Taiyuan
LA-9
Yaogan 26 SSO Success
25 26 June 2015
06:22
Taiyuan
LA-9
Gaofen 8 SSO Success
26 8 November 2015
07:06
Taiyuan
LA-9
Yaogan 28 SSO Success
27 30 May 2016
03:17
Taiyuan
LA-9
Ziyuan 3-02
ÑuSat-1/-2
SSO Success
28 29 June 2016
03:21
Jiuquan
LA-4/SLS-2
Shijian 16-02 LEO Success
29 15 June 2017
03:00
Jiuquan,
LA-4/SLS-2
HXMT
ÑuSat-3
Zhuhai-1
SSO Success
30 31 July 2018
03:00
Taiyuan
LA-9
Gaofen 11 SSO Success
31 24 October 2018
22:57
Taiyuan
LA-9
HaiYang-2B SSO Success[6]
32 29 April 2019
22:52
Taiyuan
LA-9
Tianhui-2-01 A/B SSO Success
33 12 September 2019
03:26
Taiyuan
LA-9
Ziyuan I-02D SSO Success
34 3 November 2019
03:22
Taiyuan
LA-9
Gaofen 7 SSO Success
35 20 December 2019
03:22
Taiyuan
LA-9
CBERS-4A
ETRSS-1
SSO Success
36 3 July 2020
03:10
Taiyuan
LA-9
Gaofen
BY-2
SSO Success
37 25 July 2020
03:13
Taiyuan,
LA-9
Ziyuan 3-03
Tianqi 10
Lobster Eye 1
SSO Success
Source: Gunter's Space Page[7]
gollark: Mechanical ones use different generally clickier switches.
gollark: Membrane, I think.
gollark: It lacks function keys, unlike my laptop somehow.
gollark: My brother is very gamer and has a mechanical keyboard.
gollark: Yes. Those who deny this are to "1v1" me in Factorio.

References

  1. Brian Harvey (2013). China in Space: The Great Leap Forward. Springer Science & Business Media. p. 96. ISBN 978-1-4614-5043-6.
  2. Mark Wade. "CZ-4B". Encyclopedia Astronautica. Archived from the original on 21 March 2008. Retrieved 27 April 2008.
  3. Gunter Krebs. "CZ-4B (Chang Zheng-4B)". Gunter's Space Page. Retrieved 27 April 2008.
  4. Boadle, Anthony. "China-Brazil satellite launch fails, likely fell back to Earth". Reuters. Retrieved 10 December 2013.
  5. de Selding, Peter B. (3 March 2014). "China Great Wall Pins December Long March Launch Failure on Fuel-line Clog". SpaceNews. Retrieved 10 August 2015.
  6. Barbosa, Rui C. (24 October 2018). "Chinese Long March 4B lofts Haiyang-2B". NASASpaceFlight.com. Retrieved 24 October 2018.
  7. Krebs, Gunter. "CZ-4B (Chang Zheng-4B)". Gunter's Space Page. Retrieved 25 October 2018.
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