Engineering:Long March 4B
From HandWiki
Short description: Chinese orbital launch vehicle
Rendering of Long March 4B | |
Function | Launch vehicle |
---|---|
Manufacturer | SAST |
Country of origin | China |
Cost per launch | US$50 million (2006) [1] |
Size | |
Height | 44.1 m (145 ft)[1] |
Diameter | 3.35 m (11.0 ft)[2] |
Mass | 249,200 kg (549,400 lb)[2] |
Stages | 3 |
Capacity | |
Payload to LEO | 4,200 kg (9,300 lb) [3] |
Payload to SSO | 2,800 kg (6,200 lb)[3] |
Payload to GTO | 1,500 kg (3,300 lb)[3] |
Associated rockets | |
Family | Long March |
Derivatives | Long March 4C |
Launch history | |
Status | Active |
Launch sites |
|
Total launches | 48 |
Successes | 47 |
Failures | 1 |
First flight | 10 May 1999 |
Last flight | 16 April 2023 |
First stage | |
Length | 27.91 m (91.6 ft) |
Diameter | 3.35 m (11.0 ft) |
Propellant mass | 182,000 kg (401,000 lb) |
Engines | 4 YF-21C |
Thrust | 2,961.6 kN (665,800 lbf) |
Specific impulse | 2,550 m/s (8,400 ft/s) |
Fuel | N2O4 / UDMH |
Second stage | |
Length | 10.9 m (36 ft) |
Diameter | 3.35 m (11.0 ft) |
Propellant mass | 52,700 kg (116,200 lb) |
Engines | 1 YF-24C (1 x YF-22C (Main)) (4 x YF-23C (Vernier)) |
Thrust | 742.04 kN (166,820 lbf) (Main) 47.1 kN (10,600 lbf) (Vernier) |
Specific impulse | 2,942 m/s (9,650 ft/s) (Main) 2,834 m/s (9,300 ft/s) (Vernier) |
Fuel | N2O4 / UDMH |
Third stage | |
Length | 14.79 m (48.5 ft) |
Diameter | 2.9 m (9 ft 6 in) |
Propellant mass | 14,000 kg (31,000 lb) |
Engines | 2 YF-40 |
Thrust | 100.85 kN (22,670 lbf) |
Specific impulse | 2,971 m/s (9,750 ft/s) |
Fuel | N2O4 / UDMH |
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 expendable orbital launch vehicle. Launched from Launch Complex 1 at the Taiyuan Satellite Launch Center, it is a 3-stage launch vehicle, used mostly to place satellites into low Earth orbit and Sun-synchronous orbits. It was first launched on 10 May 1999, with the FY-1C weather satellite, which would later be the target in the 2007 Chinese anti-satellite missile test.
The Chang Zheng 4B experienced its only launch failure on 9 December 2013, with the loss of the CBERS-3 satellite.[4]
Launch statistics
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List of launches
Flight number |
Serial number |
Date and time (UTC) |
Launch site | Payload | Orbit | Result |
---|---|---|---|---|---|---|
1 | Y2 | 10 May 1999 01:33 |
Taiyuan LA-7 |
Fengyun 1C Shijian 5 |
SSO | Success |
2 | Y1 | 14 October 1999 03:15 |
Taiyuan LA-7 |
CBERS-1 SACI-1 |
SSO | Success |
3 | Y3 | 1 September 2000 03:25 |
Taiyuan LA-7 |
Ziyuan II-01 | SSO | Success |
4 | Y5 | 15 May 2002 01:50 |
Taiyuan LA-7 |
Fengyun 1D HaiYang-1A |
SSO | Success |
5 | Y6 | 27 October 2002 03:17 |
Taiyuan LA-7 |
Ziyuan II-02 | SSO | Success |
6 | Y4 | 21 October 2003 03:16 |
Taiyuan LA-7 |
CBERS-2 Chuangxin 1-01 |
SSO | Success |
7 | Y7 | 8 September 2004 23:14 |
Taiyuan LA-7 |
Shijian 6-01A Shijian 6-01B |
SSO | Success |
8 | Y8 | 6 November 2004 03:10 |
Taiyuan LA-7 |
Ziyuan II-03 | SSO | Success |
9 | Y16 | 23 October 2006 23:34 |
Taiyuan LA-7 |
Shijian 6-02A Shijian 6-02B |
SSO | Success |
10 | Y17 | 19 September 2007 03:26 |
Taiyuan LA-7 |
CBERS-2B | SSO | Success |
11 | Y22 | 25 October 2008 01:15 |
Taiyuan LA-9 |
Shijian 6-03A Shijian 6-03B |
SSO | Success |
12 | Y20 | 15 December 2008 03:22 |
Taiyuan LA-9 |
Yaogan 5 | SSO | Success |
13 | Y23 | 6 October 2010 00:49 |
Taiyuan LA-9 |
Shijian 6-04A Shijian 6-04B |
SSO | Success |
14 | Y14 | 15 August 2011 22:57 |
Taiyuan LA-9 |
HaiYang-2A | SSO | Success |
15 | Y21 | 9 November 2011 03:21 |
Taiyuan LA-9 |
Yaogan 12 Tianxun 1 |
SSO | Success |
16 | Y15 | 22 December 2011 03:26 |
Taiyuan LA-9 |
Ziyuan I-02C | SSO | Success |
17 | Y26 | 9 January 2012 03:17 |
Taiyuan LA-9 |
Ziyuan 3-01 VesselSat-2 |
SSO | Success |
18 | Y12 | 10 May 2012 07:06 |
Taiyuan LA-9 |
Yaogan 14 Tiantuo 1 |
SSO | Success |
19 | Y25 | 25 October 2013 03:50 |
Jiuquan LA-4/SLS-2 |
Shijian 16-01 | LEO | Success |
20 | Y10 | 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 | Y27 | 19 August 2014 03:15 |
Taiyuan LA-9 |
Gaofen 2 BRITE-PL2 (Heweliusz) |
SSO | Success |
22 | Y28 | 8 September 2014 03:22 |
Taiyuan LA-9 |
Yaogan 21 Tiantuo 2 |
SSO | Success |
23 | Y32 | 7 December 2014 03:26 |
Taiyuan LA-9 |
CBERS-4 | SSO | Success |
24 | Y29 | 27 December 2014 03:22 |
Taiyuan LA-9 |
Yaogan 26 | SSO | Success |
25 | Y30 | 26 June 2015 06:22 |
Taiyuan LA-9 |
Gaofen 8 | SSO | Success |
26 | Y24 | 8 November 2015 07:06 |
Taiyuan LA-9 |
Yaogan 28 | SSO | Success |
27 | Y33 | 30 May 2016 03:17 |
Taiyuan LA-9 |
Ziyuan 3-02 ÑuSat-1/-2 |
SSO | Success |
28 | Y35 | 29 June 2016 03:21 |
Jiuquan LA-4/SLS-2 |
Shijian 16-02 | LEO | Success |
29 | Y31 | 15 June 2017 03:00 |
Jiuquan LA-4/SLS-2 |
HXMT ÑuSat-3 Zhuhai-1 |
LEO | Success |
30 | Y37 | 31 July 2018 03:00 |
Taiyuan LA-9 |
Gaofen 11-01 | SSO | Success |
31 | Y34 | 24 October 2018 22:57 |
Taiyuan LA-9 |
Haiyang-2B | SSO | Success[6] |
32 | Y36 | 29 April 2019 22:52 |
Taiyuan LA-9 |
Tianhui-2-01 A/B | SSO | Success |
33 | Y39 | 12 September 2019 03:26 |
Taiyuan LA-9 |
Ziyuan I-02D | SSO | Success |
34 | Y38 | 3 November 2019 03:22 |
Taiyuan LA-9 |
Gaofen 7 Xiaoxiang 1-08 |
SSO | Success |
35 | Y44 | 20 December 2019 03:22 |
Taiyuan LA-9 |
CBERS-4A ETRSS-1 |
SSO | Success |
36 | Y43 | 3 July 2020 03:10 |
Taiyuan LA-9 |
Gaofen Multi-Mode BY-70-2 |
SSO | Success |
37 | Y45 | 25 July 2020 03:13 |
Taiyuan LA-9 |
Ziyuan 3-03 Tianqi 10 NJU-HKU 1 |
SSO | Success |
38 | Y46 | 7 September 2020 05:57 |
Taiyuan LA-9 |
Gaofen 11-02 | SSO | Success |
A booster presumably coming from this launch fell near populated areas.[7][8] | ||||||
39 | Y41 | 21 September 2020 05:40 |
Jiuquan LA-4/SLS-2 |
Haiyang-2C | LEO | Success |
40 | Y42 | 27 September 2020 03:23 |
Taiyuan LA-9 |
Huanjing-2A Huanjing-2B |
SSO | Success |
41 | Y49 | 8 April 2021 23:01 |
Taiyuan LA-9 |
Shiyan 6-03 | SSO | Success |
42 | Y48 | 19 May 2021 04:03 |
Jiuquan LA-4/SLS-2 |
Haiyang-2D | LEO | Success |
43 | Y50 | 18 August 2021 22:32 |
Taiyuan LA-9 |
Tianhui-2 02A Tianhui-2 02B |
SSO | Success |
44 | Y52 | 20 November 2021 01:51 |
Taiyuan LA-9 |
Gaofen 11-03 | SSO | Success |
45 | Y47 | 10 December 2021 00:11 |
Jiuquan LA-4/SLS-2 |
Shijian-6 05A Shijian-6 05B |
SSO | Success |
46 | Y40 | 4 August 2022 03:08 |
Taiyuan LA-9 |
TECIS Minxing Shaonian Jiaotong-4 |
SSO | Success |
47 | Y55 | 27 December 2022 07:37 |
Taiyuan LA-9 |
Gaofen 11-04 | SSO | Success |
48 | Y51 | 16 April 2023 01:36 |
Jiuquan LA-4/SLS-2 |
Fengyun 3G | LEO | Success |
Source: Gunter's Space Page[9] |
See also
References
- ↑ Brian Harvey (2013). China in Space: The Great Leap Forward. Springer Science & Business Media. p. 96. ISBN 978-1-4614-5043-6. https://books.google.com/books?id=hZBAAAAAQBAJ&pg=PA96.
- ↑ 2.0 2.1 "CZ-4B". Encyclopedia Astronautica. http://www.astronautix.com/lvs/cz4b.htm.
- ↑ 3.0 3.1 3.2 "Long March-4B". Gunter's Space Page. http://space.skyrocket.de/doc_lau_det/cz-4b.htm.
- ↑ Boadle, Anthony. "China-Brazil satellite launch fails, likely fell back to Earth". https://www.reuters.com/article/space-china-brazil-satellite-idUSL1N0JO0UQ20131209.
- ↑ "China Great Wall Pins December Long March Launch Failure on Fuel-line". SpaceNews. 3 March 2014. http://spacenews.com/39687china-great-wall-pins-december-long-march-launch-failure-on-fuel-line/.
- ↑ Barbosa, Rui C. (24 October 2018). "Chinese Long March 4B lofts Haiyang-2B". NASASpaceFlight.com. https://www.nasaspaceflight.com/2018/10/chinese-long-march-4b-lofts-haiyang-2b/.
- ↑ Jones, Andrew (7 September 2020). "Chinese rocket booster appears to crash near school during Gaofen 11 satellite launch". Space.com. https://www.space.com/china-launches-gaofen-11-satellite-rocket-crash.html.
- ↑ Sebastian Kettley (8 September 2020). "China rocket crash: Watch the moment Long March booster rocket crashes near school - video". https://www.express.co.uk/news/science/1332690/China-rocket-crash-video-Long-March-4B-booster-rocket-crash-school.
- ↑ "CZ-4B (Chang Zheng-4B)". Gunter's Space Page. https://space.skyrocket.de/doc_lau_det/cz-4b.htm.
Original source: https://en.wikipedia.org/wiki/Long March 4B.
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