Long March 3B#Long March 3B/E

{{Short description|Chinese orbital carrier rocket}}

{{Use British English|date=March 2020}}

{{Use dmy dates|date=March 2020}}

{{Infobox rocket

| name = Long March 3B

| image = CZ-3B rendering.jpg

| caption = Rendering of Long March 3B

| function = Launch vehicle

| manufacturer = China Academy of Launch Vehicle Technology (CALT)

| country-origin = China

| cpl = US$50-70 million {{Cite web|url=https://www.aspistrategist.org.au/cheap-reusable-space-launchers-are-still-years-away-for-chinese-military/|title = Cheap, reusable space launchers are still years away for Chinese military|date = 24 March 2021}}{{cite web |title=How GSLV compares in the international launch market? |date=29 July 2019|url=https://www.geospatialworld.net/blogs/how-gslv-compares-in-the-international-launch-market/}}{{cite web |title=Long March 3B |url=https://rocketrundown.com/home/rocket-index/china-academy-of-launch-vehicle-technology-calt/long-march-3b-calt/}}

| height = {{plainlist|

  • 3B: {{cvt|54.8|m}} {{cite web|url=http://www.astronautix.com/lvs/cz3b.htm|title=CZ-3B|author=Mark Wade|publisher=Encyclopedia Astronautica|access-date=26 April 2008|url-status=dead |archiveurl=https://web.archive.org/web/20080319040124/http://www.astronautix.com/lvs/cz3b.htm|archive-date=19 March 2008}}
  • 3B/E: {{cvt|56.3|m}} {{cite web|url=http://www.cgwic.com/LaunchServices/LaunchVehicle/LM3B.html|title=LM-3B|publisher=China Great Wall Industry Corporation|access-date=23 May 2012|archive-date=10 June 2012|archive-url=https://web.archive.org/web/20120610043108/http://www.cgwic.com/LaunchServices/LaunchVehicle/LM3B.html|url-status=dead}}

}}

| diameter = {{cvt|3.35|m}}

| mass = {{plainlist|

  • 3B: {{cvt|425800|kg}}
  • 3B/E: {{cvt|458970|kg}}

}}

| stages = 3 / 4

| capacities =

{{Infobox rocket/payload

| location = LEO

| kilos = {{cvt|11500|kg}} {{cite web|url=http://www.cgwic.com/LaunchServices/Download/manual/LM-3A%20Series%20Launch%20Vehicles%20User's%20Manual%20Issue%202011.pdf |title=LM-3A Series Launch Vehicle User's Manual - Issue 2011|publisher=China Great Wall Industries Corporation|access-date=2015-08-09|url-status=dead |archiveurl=https://web.archive.org/web/20150717190345/http://www.cgwic.com/LaunchServices/Download/manual/LM-3A%20Series%20Launch%20Vehicles%20User%27s%20Manual%20Issue%202011.pdf|archive-date=2015-07-17}}{{cite web|url=http://space.skyrocket.de/doc_lau_det/cz-3b.htm|title=CZ-3B (Chang Zheng-3B)|author=Gunter Krebs|publisher=Gunter's Space Page|access-date=26 April 2008}}

}}

{{Infobox rocket/payload

| location = SSO

| kilos = {{cvt|7100|kg}}

}}

{{Infobox rocket/payload

| location = GTO

| kilos = {{plainlist|

  • 3B: {{cvt|5100|kg}}
  • 3B/E: {{cvt|5500|kg}}

}}

}}

{{Infobox rocket/payload

| location = GEO

| kilos = {{cvt|2000|kg}}

}}

{{Infobox rocket/payload

| location = HCO

| kilos = {{cvt|3300|kg}}

}}

| family = Long March

| derivatives = Long March 3C

| comparable = {{flatlist|

}}

| status = {{plainlist|

  • 3B: Retired
  • 3B/E: Active

}}

| sites = Xichang LC-2, LC-3

| launches = {{flatlist|

  • 110
  • 3B: 12
  • 3B/E: 98

}}

| success = {{flatlist|

  • 106
  • 3B: 10
  • 3B/E: 96

}}

| fail = {{flatlist|

}}

| partial = {{flatlist|

}}

| first = {{plainlist|

}}

| last = {{plainlist|

}}

|payloads = {{flatlist|Chang'e 3, Chang'e 4, BeiDou, ChinaSat, Tianwen-2

}}

| stagedata = {{Infobox rocket/stage

| type = booster

| diff = 3B

| number = 4

| length = {{cvt|15.33|m}}

| diameter = {{cvt|2.25|m}}

| empty =

| gross =

| propmass = {{cvt|37700|kg}}

| engines = 1 × YF-25

| thrust = {{cvt|740.4|kN}}

| SI = {{cvt|2556.2|m/s|isp}}

| burntime = 127 seconds

| fuel = N2O4 / UDMH

}}

{{Infobox rocket/stage

| type = booster

| diff = 3B/E

| number = 4

| length = {{cvt|16.1|m}}

| diameter = {{cvt|2.25|m}}

| empty =

| gross =

| propmass = {{cvt|41100|kg}}

| engines = 1 × YF-25

| thrust = {{cvt|740.4|kN}}

| SI = {{cvt|2556.2|m/s|isp}}

| burntime = 140 seconds

| fuel = N2O4 / UDMH

}}

{{Infobox rocket/stage

| type = stage

| stageno = First

| diff = 3B

| length = {{cvt|23.27|m}}

| diameter = {{cvt|3.35|m}}

| empty =

| gross =

| propmass = {{cvt|171800|kg}}

| engines = 4 × YF-21C

| thrust = {{cvt|2961.6|kN}}

| SI = {{cvt|2556.5|m/s|isp}}

| burntime = 145 seconds

| fuel = N2O4 / UDMH

}}

{{Infobox rocket/stage

| type = stage

| stageno = First

| diff = 3B/E

| length = {{cvt|24.76|m}}

| diameter = {{cvt|3.35|m}}

| empty =

| gross =

| propmass = {{cvt|186200|kg}}

| engines = 4 × YF-21C

| thrust = {{cvt|2961.6|kN}}

| SI = {{cvt|2556.5|m/s|isp}}

| burntime = 158 seconds

| fuel = N2O4 / UDMH

}}

{{Infobox rocket/stage

| type = stage

| stageno = Second

| length = {{cvt|12.92|m}}

| diameter = {{cvt|3.35|m}}

| empty =

| gross =

| propmass = {{cvt|49400|kg}}

| engines = {{flatlist|

}}

| thrust = {{plainlist|

  • {{cvt|742|kN}} (Main)
  • {{cvt|47.1|kN}} (Vernier)

}}

| SI = {{plainlist|

  • {{cvt|2922.57|m/s}} (Main)
  • {{cvt|2910.5|m/s}} (Vernier)

}}

| burntime = 185 seconds

| fuel = N2O4 / UDMH

}}

{{Infobox rocket/stage

| type = stage

| stageno = Third

| length = {{cvt|12.38|m}}

| diameter = {{cvt|3.0|m}}

| empty =

| gross =

| propmass = {{cvt|18200|kg}}

| engines = 2 × YF-75

| thrust = {{cvt|167.17|kN}}

| SI = {{cvt|4295|m/s|isp}}

| burntime = 478 seconds

| fuel = {{LH2|LH2}} / LOX

}}

{{Infobox rocket/stage

| type = stage

| stageno = Fourth

| diff = optional

| name = YZ-1

| engines = 1 × YF-50D

| thrust = {{cvt|6.5|kN}}

| SI = {{cvt|315.5|isp}}

| burntime =

| fuel = N2O4 / UDMH

}}

}}

The Long March 3B ({{zh|c=长征三号乙|p=Chángzhēng sānhàoyǐ}}), also known as the CZ-3B and LM-3B, is a Chinese orbital launch vehicle. Introduced in 1996, it is launched from Launch Area 2 and 3 at the Xichang Satellite Launch Center in Sichuan. A three-stage rocket with four strap-on liquid rocket boosters, it is the heaviest variant of the Long March 3 rocket family, and is mainly used to place communications satellites and navigation satellites into geosynchronous orbits.

An enhanced version, the Long March 3B/E or G2, was introduced in 2007 to increase the rocket's geostationary transfer orbit (GTO) cargo capacity and lift heavier geosynchronous orbit (GEO) communications satellites. The Long March 3B also served as the basis for the medium-capacity Long March 3C, which was first launched in 2008.

{{As of|2025|5|28}}, the Long March 3B, 3B/E and 3B/G5 have conducted 105 successful launches, plus 2 failures and 2 partial failures, accumulating a success rate of {{percent|105|109|1}}. It is the first Long March series rocket to accumulate 100 orbital launches.

History

The development of the Long March 3B began in 1986 to meet the needs of the international GEO communications satellite market. During its maiden flight, on 14 February 1996 carrying the Intelsat 708 satellite, the rocket suffered a guidance failure two seconds into the flight and destroyed a nearby town, killing at least six people,{{cite web|url=http://www.house.gov/coxreport/body/ch6bod.html |title=Satellite Launches in the PRC: Loral|access-date=23 May 2012|author=Select Committee of the United States House of Representatives|date=3 January 1999|publisher=U.S. National Security and Military/Commercial Concerns with the People's Republic of China}} {{PD-notice}} but outside estimates suggest that anywhere between 200 and 500 people might have been killed.{{cite web |last=Lan|first=Chen|title=Mist around the CZ-3B disaster|url=http://www.thespacereview.com/article/2323/1|publisher=The Space Review|access-date=18 January 2014}} However, the author of the report later ruled out large casualties, because evidence suggest that the crash site was evacuated before the launch.{{cite web|last=Lan|first=Chen|title=Mist around the CZ-3B disaster (part 2)|url=http://www.thespacereview.com/article/2326/1|publisher=The Space Review|access-date=29 October 2014}}

The Long March 3B and 3B/E rockets conducted ten successful launches between 1997 and 2008.

In 1997, the Agila 2 satellite was forced to use onboard propellant to reach its correct orbit because of poor injection accuracy on the part of its Long March 3B launch vehicle.International reference guide to space launch systems. Fourth edition. p. 243. {{ISBN|1-56347-591-X}} In 2009, a Long March 3B partially failed during launch due to a third stage anomaly, which resulted in the Palapa-D satellite reaching a lower orbit than planned.{{cite web|url=http://news.xinhuanet.com/mil/2009-08/31/content_11973441.htm|archive-url=https://web.archive.org/web/20090904032008/http://news.xinhuanet.com/mil/2009-08/31/content_11973441.htm|url-status=dead|archive-date=4 September 2009|title="帕拉帕-D"通信卫星未能进入预定轨道|publisher=Xinhuanet|date=31 August 2009|access-date=31 August 2009}} Nonetheless, the satellite was able to maneuver itself into the planned orbit. The Long March 3B and its variants remain in active use {{as of|2021|01|lc=y}}, having conducted a total of 26 consecutive successful launches, since 19 June 2017 until 9 March 2020.

In December 2013, a Long March 3B/E successfully lifted Chang'e 3, China's first Lunar lander and rover into the projected lunar-transfer orbit.

In April 2020, the third stage of the Long March 3B/E failed during a Palapa-N1 communications satellite mission; this was the first total failure of the Long March 3B/E.{{cite web |url=https://www.nasaspaceflight.com/2020/04/long-march-3b-launches-indonesian-satellite/|title=Long March 3B fails during Indonesian satellite launch|last=Barbosa|first=Rui C.|date=2020-04-09 |publisher=NASASpaceFlight.com|access-date=2020-04-09}}

Design and variants

The Long March 3B is based on the Long March 3A as its core stage, with four liquid boosters strapped on the first stage. It has a low Earth orbit (LEO) cargo capacity of {{cvt|11200|kg}} and a GTO capacity is {{cvt|5100|kg}}.

= Long March 3B/E =

The Long March 3B/E, also known as 3B/G2, is an enhanced variant of the Long March 3B, featuring an enlarged first stage and boosters, increasing its GTO payload capacity to {{cvt|5500|kg}}.{{cite web|url=http://www.cgwic.com/LaunchServices/LaunchVehicle/LM3B.html|title=LM-3B|publisher=China Great Wall Industry Corporation|access-date=31 August 2009|archive-date=10 June 2012|archive-url=https://web.archive.org/web/20120610043108/http://www.cgwic.com/LaunchServices/LaunchVehicle/LM3B.html|url-status=dead}} Its maiden flight took place on 13 May 2007, when it successfully launched Nigeria's NigComSat-1, the first African geosynchronous communications satellite. In 2013, it successfully launched China's first lunar lander Chang'e 3 and lunar rover Yutu.

Since 2015, the Long March 3B and 3C can optionally accommodate a YZ-1 upper stage, which has been used to carry dual launches or BeiDou navigation satellites into medium Earth orbit (MEO).

= Long March 3C =

{{main|Long March 3C}}

A modified version of the Long March 3B, the Long March 3C, was developed in the mid-1990s to bridge the gap in payload capacity between the Long March 3B and 3A. It is almost identical to the Long March 3B, but has two boosters instead of four, giving it a reduced GTO payload capacity of {{cvt|3800|kg}}. Its maiden launch took place on 25 April 2008.

Launch statistics

{{#invoke:Chart | bar chart

| height = 300

| width = 800

| stack = 1

| group 1 = 1: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 1: 0: 0: 0: 0: 0

| group 2 = 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 1: 0: 0: 0: 0: 0: 0: 0: 1: 0: 0: 0: 0: 0: 0: 0: 0

| group 3 = 0: 2: 2: 0: 0: 0: 0: 0: 0: 1: 1: 2: 2: 0: 1: 5: 5: 3: 0: 8: 3: 4: 11: 11: 7: 11: 4: 6: 8: 9

| group 4 = 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 0: 3

| colors = FireBrick : Orange : ForestGreen : LightBlue

| group names = Failure : Partial failure : Success : Planned

| units suffix = _launches

| x legends = 1996 :::: 2000 ::::: 2005 ::::: 2010 ::::: 2015 ::::: 2020 ::::: 2025

}}

List of launches

{{main|List of Long March launches}}

class="wikitable"

! Flight number

! Serial number

! Date (UTC)

! Launch site

! Version

! Payload

! Orbit

! Result

1

| Y1

| 14 February 1996
19:01

| XSLC, LA-2

| 3B

| Intelsat 708

| GTO

| {{Failure|Failure}}

2

| Y2

| 19 August 1997
17:50

| XSLC, LA-2

| 3B

| Agila-2

| GTO

| {{Success}}

3

| Y3

| 16 October 1997
19:13

| XSLC, LA-2

| 3B

| APStar 2R

| GTO

| {{Success}}

4

|Y5

|30 May 1998
10:00

|XSLC, LA-2

|3B

|Chinastar 1

|GTO

|{{Success}}

5

|Y4

|18 July 1998
09:20

|XSLC, LA-2

|3B

|SinoSat 1

|GTO

|{{Success}}

6

|Y6

|12 April 2005
12:00

|XSLC, LA-2

|3B

|APStar 6

|GTO

|{{Success}}

7

|Y7

|28 October 2006
16:20

|XSLC, LA-2

|3B

|SinoSat 2

|GTO

|{{Success}}

8

|Y9

|13 May 2007
16:01

|XSLC, LA-2

|3B/E

|NigComSat-1

|GTO

|{{Success}}

9

|Y10

|5 July 2007
12:08

|XSLC, LA-2

|3B

|ChinaSat 6B

|GTO

|{{Success}}

10

|Y11

|9 June 2008
12:15

|XSLC, LA-2

|3B

|ChinaSat 9

|GTO

|{{Success}}

11

|Y12

|29 October 2008
16:53

|XSLC, LA-2

|3B/E

|Venesat-1

|GTO

|{{Success}}

12

|Y8

|31 August 2009
09:28

|XSLC, LA-2

|3B

|Palapa-D

|GTO

|{{Partial failure|Partial Failure}}

13

|Y13

|4 September 2010
16:14

|XSLC, LA-2

|3B/E

|SinoSat 6

|GTO

|{{Success}}

14

|Y20

|20 June 2011
16:13

|XSLC, LA-2

|3B/E

|ChinaSat 10

|GTO

|{{Success}}

15

|Y19

|11 August 2011
16:15

|XSLC, LA-2

|3B/E

|Paksat-1R

|GTO

|{{Success}}

16

|Y16

|18 September 2011
16:33

|XSLC, LA-2

|3B/E

|ChinaSat 1A

|GTO

|{{Success}}

17

|Y18

|7 October 2011
08:21

|XSLC, LA-2

|3B/E

|Eutelsat W3C

|GTO

|{{Success}}

18

|Y21

|19 December 2011
16:41

|XSLC, LA-2

|3B/E

|NigComSat-1R

|GTO

|{{Success}}

19

|Y22

|31 March 2012
10:27

|XSLC, LA-2

|3B/E

|APStar 7

|GTO

|{{Success}}

20

|Y14

|29 April 2012
20:50

|XSLC, LA-2

|3B

|Compass-M3
Compass-M4

|MEO

|{{Success}}

21

|Y17

|26 May 2012
15:56

|XSLC, LA-2

|3B/E

|ChinaSat 2A

|GTO

|{{Success}}

22

|Y15

|18 September 2012
19:10

|XSLC, LA-2

|3B

|Compass-M5
Compass-M6

|MEO

|{{Success}}

23

|Y24

|27 November 2012
10:13

|XSLC, LA-2

|3B/E

|ChinaSat 12

|GTO

|{{Success}}

24

|Y25

|1 May 2013
16:06

|XSLC, LA-2

|3B/E

|ChinaSat 11

|GTO

|{{Success}}

25

|Y23

|1 December 2013
17:30

|XSLC, LA-2

|3B/E

|Chang'e 3

|TLI

|{{Success}}

26

|Y27

|20 December 2013
16:42

|XSLC, LA-2

|3B/E

|Túpac Katari 1

|GTO

|{{Success}}

27

|Y26

|25 July 2015
12:29

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou M1-S
BeiDou M2-S

|MEO

|{{Success}}

28

|Y32

|12 September 2015
15:42

|XSLC, LA-2

|3B/E

|TJS-1

|GTO

|{{Success}}

29

|Y33

|29 September 2015
23:13

|XSLC, LA-3

|3B/E

|BeiDou I2-S

|GTO

|{{Success}}

30

|Y36

|16 October 2015
16:16

|XSLC, LA-2

|3B/E

|APStar 9

|GTO

|{{Success}}

31

|Y34

|3 November 2015
16:25

|XSLC, LA-3

|3B/E

|ChinaSat 2C

|GTO

|{{Success}}

32

|Y38

|20 November 2015
16:07

|XSLC, LA-2

|3B/E

|LaoSat-1

|GTO

|{{Success}}

33

|Y31

|9 December 2015
16:46

|XSLC, LA-3

|3B/E

|ChinaSat 1C

|GTO

|{{Success}}

34

|Y37

|28 December 2015
16:04

|XSLC, LA-2

|3B/E

|Gaofen 4

|GTO

|{{Success}}

35

|Y29

|15 January 2016
16:57

|XSLC, LA-3

|3B/E

|Belintersat-1

|GTO

|{{Success}}

36

|Y35

|5 August 2016
16:22

|XSLC, LA-3

|3B/E

|Tiantong 1-01

|GTO

|{{Success}}

37

|Y42

|10 December 2016
16:11

|XSLC, LA-3

|3B/E

|Fengyun-4A

|GTO

|{{Success}}

38

|Y39

|5 January 2017
15:18

|XSLC, LA-2

|3B/E

|TJS-2

|GTO

|{{Success}}

39

|Y43

|12 April 2017
11:04

|XSLC, LA-2

|3B/E

|Shijian 13

|GTO

|{{Success}}

40

|Y28

|19 June 2017
16:11

|XSLC, LA-2

|3B/E

|Chinasat 9A

|GTO

|{{Partial failure|Partial failure}}

41

|Y46

|5 November 2017
11:45

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou-3 M1
BeiDou-3 M2

|MEO

|{{Success}}

42

|Y40

|10 December 2017
16:40

|XSLC, LA-2

|3B/E

|Alcomsat-1

|GTO

|{{Success}}

43

|Y45

|11 January 2018
23:18

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou-3 M7
BeiDou-3 M8

|MEO

|{{Success}}

44

|Y47

|12 February 2018
05:03

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou-3 M3
BeiDou-3 M4

|MEO

|{{Success}}

45

|Y48

|29 March 2018
17:56

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou-3 M9
BeiDou-3 M10

|MEO

|{{Success}}

46

|Y55

|3 May 2018
16:06

|XSLC, LA-2

|3B/E

|Apstar 6C

|GTO

|{{Success}}

47

|Y49

|29 July 2018
01:48

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M5
BeiDou-3 M6

|MEO

|{{Success}}

48

|Y50

|24 August 2018
23:52

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M11
BeiDou-3 M12

|MEO

|{{Success}}

49

|Y51

|19 September 2018
14:07

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M13
BeiDou-3 M14

|MEO

|{{Success}}

50

|Y52

|15 October 2018
04:23

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M15
BeiDou-3 M16

|MEO

|{{Success}}

51

|Y41

|1 November 2018
15:57

|XSLC, LA-2

|3B/E

|BeiDou-3 G1

|GTO

|{{Success}}

52

|Y53

|18 November 2018
18:07

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M17
BeiDou-3 M18

|MEO

|{{Success}}

53

|Y30

|7 December 2018
18:23

|XSLC, LA-2

|3B/E

|Chang'e 4

|TLI

|{{Success}}

54

|Y56

|10 January 2019
17:11

|XSLC, LA-2

|3B/E

|ChinaSat 2D

|GTO

|{{Success}}

55

|Y54

|9 March 2019
16:28

|XSLC, LA-3

|3B/E

|ChinaSat 6C

|GTO

|{{Success}}

56

|Y44

|31 March 2019
15:51

|XSLC, LA-2

|3B/E

|Tianlian 2-01

|GTO

|{{Success}}

57

|Y59

|20 April 2019
14:41

|XSLC, LA-3

|3B/E

|BeiDou-3 I1

|GTO

|{{Success}}

58

|Y60

|24 June, 2019
18:09

|XSLC, LA-3

|3B/E

|BeiDou-3 I2

|GTO

|{{Success}}

59

|Y58

|19 August 2019
12:03

|XSLC, LA-2

|3B/E

|ChinaSat 18

|GTO

|{{Success}}

60

|Y65

|22 September 2019
21:10

|XSLC, LA-2

|3B/E + YZ-1

|BeiDou-3 M23
BeiDou-3 M24

|MEO

|{{Success}}

61

|Y57

|17 October 2019
15:21

|XSLC, LA-3

|3B/E

|TJS-4

|GTO

|{{Success}}

62

|Y61

|4 November 2019
17:43

|XSLC, LA-2

|3B/E

|BeiDou-3 I3

|GTO

|{{Success}}

63

|Y66

|23 November 2019
00:55

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M21
BeiDou-3 M22

|MEO

|{{Success}}

64

|Y67

|16 December 2019
07:22

|XSLC, LA-3

|3B/E + YZ-1

|BeiDou-3 M19
BeiDou-3 M20

|MEO

|{{Success}}

65

| Y62

| 7 January 2020
15:20

| XSLC, LA-2

| 3B/E

| TJS-5

| GTO

| {{Success}}

66

| Y69

| 9 March 2020
11:55

| XSLC, LA-2

| 3B/E

| BeiDou-3 G2

| GTO

| {{Success}}

67

| Y71

| 9 April 2020
11:46

| XSLC, LA-2

| 3B/E

| Palapa-N1 (Nusantara Dua)

| GTO

| {{Failure|Failure}} {{cite web|url=http://www.xinhuanet.com/2020-04/09/c_1125834989.htm|title=PALAPA-N1卫星发射失利|last=Jing|first=Zhan|date=9 April 2020|website=xinhuanet.com}}

68

| Y68

| 23 June 2020
01:43 {{cite web|url=https://spaceflightnow.com/launch-schedule/|title=Launch Schedule|publisher=Spaceflight Now|date=22 June 2020|access-date=22 June 2020}}

| XSLC, LA-2

| 3B/E

| BeiDou-3 G3

| GTO

| {{Success}}

69

| Y64

| 9 July 2020
12:11 {{cite web|url=https://spaceflightnow.com/2020/07/09/commercial-high-throughput-communications-satellite-launched-from-china/|title=High-throughput communications satellite launched from China|publisher=Spaceflight Now|date=9 July 2020|access-date=10 July 2020}}

| XSLC, LA-2

| 3B/E

| Apstar 6D

| GTO

| {{Success}}

70

| Y63

| 11 October 2020
16:57 {{cite web|url=https://spacenews.com/china-launches-gaofen-13-observation-satellite-towards-geostationary-orbit/|title=China launches Gaofen-13 observation satellite towards geostationary orbit|publisher=SpaceNews|date=11 October 2020|access-date=12 October 2020}}

| XSLC, LA-2

| 3B/E

| Gaofen-13

| GTO

| {{Success}}

71

| Y73

| 12 November 2020
15:59 {{cite web|last=Barbosa|first=Rui C.|date=2020-11-12|title=Long March 3B lofts second Tiantong-1 spacecraft|url=https://www.nasaspaceflight.com/2020/11/long-march-3b-second-tiantong-1/|access-date=2020-11-13|website=nasaspaceflight.com}}

| XSLC, LA-2

| 3B/E

| Tiantong 1-02

| GTO

| {{Success}}

72

| Y70

| 6 December 2020
03:58

| XSLC, LA-3

| 3B/E

| Gaofen-14

| SSO

| {{Success}}

73

| Y74

| 19 January 2021
16:25

| XSLC, LA-2

| 3B/E

| Tiantong 1-03

| GTO

| {{Success}}

74

| Y77

| 4 February 2021
15:36

| XSLC, LA-3

| 3B/E

| TJS-6

| GTO

| {{Success}}

75

| Y72

| 2 June 2021
16:17

| XSLC, LA-2

| 3B/E

| Fengyun 4B

| GTO

| {{Success}}

76

| Y76

| 5 August 2021
16:30

| XSLC, LA-2

| 3B/E

| ChinaSat 2E

| GTO

| {{Success}}

77

| Y78

| 24 August 2021
15:41

| XSLC, LA-3

| 3B/E

| TJS-7

| GTO

| {{Success}}

78

| Y86

| 9 September 2021
11:50

| XSLC, LA-2

| 3B/E

| ChinaSat 9B

| GTO

| {{Success}}

79

| Y81

| 27 September 2021
08:20

| XSLC, LA-2

| 3B/E

| Shiyan 10

| GTO

| {{Success}}{{cite web|url=https://www.nasaspaceflight.com/2021/10/shiyan-10-fails-in-orbit-after-launch/|title=Chinese Shiyan-10 satellite raises its orbit after initial problems|last=Beil|first=Adrian |publisher=NASASpaceFlight.com|date=17 October 2021|access-date=18 October 2021}}

80

| Y83

| 24 October 2021
01:27:03

| XSLC, LA-2

| 3B/E

| Shijian-21

| GTO

| {{Success}}

81

| Y79

| 26 November 2021
16:40:04

| XSLC, LA-2

| 3B/E

| ChinaSat 1D

| GTO

| {{Success}}

82

| Y82

| 13 December 2021
16:09

| XSLC, LA-3

| 3B/E

| Tianlian II-02

| GTO

| {{Success}}

83

| Y84

| 29 December 2021
16:43

| XSLC, LA-2

| 3B/E

| TJS-9

| GTO

| {{Success}}

84

| Y89

| 15 April 2022
12:00

| XSLC, LA-2

| 3B/E

| ChinaSat 6D

| GTO

| {{Success}}

85

| Y85

| 12 July 2022
16:30

| XSLC, LA-2

| 3B/E

| Tianlian II-03

| GTO

| {{Success}}

86

| Y91

| 5 November 2022
11:50

| XSLC, LA-2

| 3B/E

| ChinaSat 19

| GTO

| {{Success}}

87

| Y88

| 29 December 2022
04:43

| XSLC, LA-2

| 3B/E

| Shiyan 10-02

| GTO

| {{Success}}

88

| Y93

| 23 February 2023
11:49

| XSLC, LA-2

| 3B/E

| ChinaSat 26

| GTO

| {{Success}}

89

| Y90

| 17 March 2023
08:33

| XSLC, LA-2

| 3B/E

| Gaofen 13-02

| GTO

| {{Success}}

90

| Y87

| 17 May 2023
02:49

| XSLC, LA-2

| 3B/E

| BeiDou-3 G4

| GTO

| {{Success}}

91

| Y92

| 12 August 2023
17:26

| XSLC, LA-2

| 3B/E

| Ludi Tance-4 01A

| GTO

| {{Success}}

92

| Y94

| 9 November 2023
11:23

| XSLC, LA-2

| 3B/E

| ChinaSat 6E

| GTO

| {{Success}}

93

| Y75

| 26 December 2023
03:26

| XSLC, LA-2

| 3B/E + YZ-1

| BeiDou-3 M26
BeiDou-3 M28

| MEO

| {{Success}}

94

| Y95

| 29 February 2024
13:03

| XSLC, LA-2

| 3B/E

| Weixing Hulianwang Gaogui-01

| GTO

| {{Success}}

95

| Y96

| 9 May 2024
01:43

| XSLC, LA-2

| 3B/E

| Zhihui Tianwang 1-01A
Zhihui Tianwang 1-01B

| MEO

| {{Success}}

96

| Y98

| 30 May 2024
12:12

| XSLC, LA-2

| 3B/E

| Paksat-MM1R

| GTO

| {{Success}}

97

| Y97

| 1 August 2024
13:14

| XSLC, LA-2

| 3B/E

| Weixing Hulianwang Gaogui-02

| GTO

| {{Success}}

98

| Y80

| 19 September 2024
01:14

| XSLC, LA-2

| 3B/E + YZ-1

| BeiDou-3 M25
BeiDou-3 M27

| MEO

| {{Success}}

99

| Y100

| 10 October 2024
13:50

| XSLC, LA-2

| 3B/E

| Weixing Hulianwang Gaogui-03

| GTO

| {{Success}}

100

| Y103

| 3 December 2024
05:56

| XSLC, LA-3

| 3B/E

| TJS-13

| GTO

| {{Success}}

101

| Y99

| 20 December 2024
15:12

| XSLC, LA-2

| 3B/E

| TJS-12

| GTO

| {{Success}}

102

| Y104

| 6 January 2025
20:00

| XSLC, LA-3

| 3B/E

| Shijian-25

| GTO

| {{Success}}

103

| Y105

| 23 January 2025
15:32

| XSLC, LA-2

| 3B/E

| TJS-14

| GTO

| {{Success}}

104

| Y101

| 22 February 2025
12:11

| XSLC, LA-2

| 3B/E

| ChinaSat 10R

| GTO

| {{Success}}

105

| Y107

| 9 March 2025
17:17

| XSLC, LA-3

| 3B/E

| TJS-15

| GTO

| {{Success}}

106

| Y102

| 26 March 2025
15:55

| XSLC, LA-2

| 3B/E

| Tianlian II-04

| GTO

| {{Success}}

107

| Y108

| 10 April 2025
16:47

| XSLC, LA-3

| 3B/E

| TJS-17

| GTO

| {{Success}}

108

| Y109

| 27 April 2025
15:54

| XSLC, LA-2

| 3B/E

| Tianlian II-05

| GTO

| {{Success}}

109

| Y110

| 28 May 2025
17:31

| XSLC, LA-2

| 3B/E

| Tianwen-2

| Heliocentric

| {{Success}}

110

| Y111

| 20 June 2025
12:37

| XSLC, LA-2

| 3B/E

| ChinaSat 9C

| GTO

| {{Success}}

111

| Y?

| July 2025

| XSLC, LA-2

| 3B/E

| TBA

| GTO

| {{Planned}}

112

| Y?

| July 2025

| XSLC, LA-2

| 3B/E

| TBA

| GTO

| {{Planned}}

| Y?

| September 2025

| XSLC, LA-2

| 3B/E

| Fengyun 4C

| GTO

| {{Planned}}

| Y?

| 2027

| XSLC, LA-2

| 3B/E

| ChinaSat 27

| GTO

| {{Planned}}

= Notable payloads =

Flight mishaps and anomalies

= Intelsat 708 launch failure =

{{Main|Intelsat 708}}

On 14 February 1996, the launch of the first Long March 3B with Intelsat 708 failed just after liftoff when the launch vehicle veered off course and exploded when it hit the ground at T+23 seconds.

The Xinhua news agency reported that six people were killed and 57 injured. However, the Americans on hand for the launch have testified that "dozens, if not hundreds", of people were seen to gather outside the centre's main gate near the crash site the night before launch. When reporters were being taken away from the site, they found that most buildings had sustained serious damage or had been flattened completely.{{cite web|last=Lan|first=Chen|title=Mist around the CZ-3B disaster, Part 1|url=http://www.thespacereview.com/article/2323/1|publisher=The Space Review|access-date=18 January 2014}} Other eyewitnesses were noted as having seen dozens of ambulances and many flatbed trucks, loaded with what could have been human remains, being taken to the local hospital.

The cause of the accident was traced to short-circuiting of the vehicle's guidance platform at liftoff.{{cite news|url=http://edition.cnn.com/ALLPOLITICS/resources/1999/coxreport/satellite/pg1.html|title=Satellite Launches in the PRC: Loral|publisher=CNN|access-date= 8 August 2018|date=25 May 1999}}

The participation of Space Systems/Loral in the accident investigation caused great political controversy in the United States. In 1997, the U.S. Defense Technology Security Administration found that China had obtained "significant benefit" from the Review Committee, results of which would improve their "launch vehicles ... ballistic missiles and in particular their guidance systems".

As a result, the U.S. Congress reclassified satellite technology as a munition and placed it back under the restrictive International Traffic in Arms Regulations in 1998.{{cite news|title=A short history of export control policy|url=http://www.thespacereview.com/article/528/1 |last1=Zelnio|first1=Ryan|publisher=The Space Review|date=January 9, 2006}} No license to launch United States spacecraft on Chinese rockets has been approved by the U.S. State Department since then, and an official at the Bureau of Industry and Security emphasized in 2016 that "no U.S.-origin content, regardless of significance, regardless of whether it's incorporated into a foreign-made item, can go to China".{{cite news|title=U.S. ITAR satellite export regime's effects still strong in Europe|url=http://spacenews.com/u-s-itar-satellite-export-regimes-effects-still-strong-in-europe/|last1=de Selding|first1=Peter B.|publisher=SpaceNews|date=April 14, 2016}}

= Palapa-D partial launch failure =

On 31 August 2009, during the launch of Palapa-D, the third stage engine under-performed and placed the satellite into a lower than planned orbit. The satellite was able to make up the performance shortfall using its own engine and reach geosynchronous orbit, but with its lifetime shortened to 10.5 years from the originally projected 15–16 years. The investigation found that the failure was due to burn-through of the engine's gas generator, and that "the most likely cause of the burn-through was a foreign matter or humidity-caused icing in the engine's liquid-hydrogen injectors".{{cite web|last1=de Selding |first1=Peter B.|title=Burn-through Blamed in China Long March Mishap|url=http://spacenews.com/burn-through-blamed-china-long-march-mishap/|publisher=SpaceNews|date=19 November 2009|access-date=10 August 2015}}

= ChinaSat-9A partial launch failure =

On 19 June 2017, a Long March 3B/E mission carrying ChinaSat-9A ended in partial failure. Officials did not release details regarding the status of the mission for at least 4 hours after liftoff.{{Cite web|url=http://spaceflight101.com/long-march-3b-zhongxing-9a-launch/|title=Zhongxing-9A Comsat lifts off atop Chinese Long March 3B, Launch Outcome Unclear – Spaceflight101|date=18 June 2017 }} Two weeks later, on 7 July 2017, officials confirmed that the mission had been anomalous, with Space Daily reporting that "an anomaly was found on the carrier rocket's rolling control thruster, part of the attitude control engine, during the third gliding phase". The failure in the rocket's third stage left the payload in a lower than intended orbit, and the payload was forced to spend two weeks reaching its intended orbit under its own power.{{cite web |url=http://www.spacedaily.com/reports/Chinese_satellite_Zhongxing_9A_enters_preset_orbit_999.html|title=Chinese satellite Zhongxing-9A|publisher=Space Daily}}

= Palapa-N1 (Nusantara Dua) launch failure =

On 9 April 2020, a Long March 3B launcher failed after lifting off from the Xichang Satellite Launch Center in the southwestern Sichuan province at 11:46 UTC during the launch of an Indonesian communications satellite, Palapa-N1 (Nusantara Dua) of a mass of 5500 kg and was expected to enter service in geostationary orbit at 113.0° East, replacing the Palapa-D satellite. But one of the two YF-75 third stage engines failed to ignite, preventing the Palapa-N1 (Nusantara Dua) satellite from reaching orbit.{{Cite web|url=https://kumparan.com/kumparantech/satelit-nusantara-dua-gagal-mengorbit-siaran-tv-dan-radio-terancam-bermasalah-1tCCDi3iDLY|title=Satelit Nusantara Dua Gagal Mengorbit, Siaran TV dan Radio Terancam Bermasalah}} Wreckage from the third stage and the Palapa-N1 spacecraft re-entered the atmosphere, leading to sightings of fiery debris in the skies over Guam. With the Long March 3B failure, Chinese rockets have faltered on two missions in less than a month. A Long March 7A rocket failed to place a satellite in orbit on 16 March 2020 after taking off from the Wenchang Spacecraft Launch Site on Hainan Island, located in southern China.https://spaceflightnow.com/2020/04/09/chinese-rocket-fails-during-launch-of-indonesian-communications-satellite/ - 9 April 2020 After two Chinese launch failures in less than a month, further Chinese launches will be likely delayed until it is sure that the quality control is satisfactory.{{Cite web|url=https://www.seradata.com/china-loses-another-long-march-3b-launch-fails-and-palapa-n1-falls-into-drink/|title = China loses another: Long March 3B launch fails and Palapa-N1 falls into the drink|date = 9 April 2020}}

Rocket debris

Debris from Long March 3B launches have fallen on nearby villages due to the inland location of China's launch sites. Grid fins for guiding boosters down to Earth more accurately have been tested on Long March 2C and 4B, but not yet on 3B.{{cite web|last=Li|first=Michael Sheetz,Yun|date=2019-11-26|title='Adjust your location quickly' — How China warns residents before rockets crash down from space |url=https://www.cnbc.com/2019/11/26/chinese-rocket-crushes-houses-after-government-warning-to-residents.html|access-date=2020-08-04|website=cnbc.com}}

See also

{{Portal|Spaceflight|China}}

References

{{Portal|Spaceflight|China}}

{{Reflist}}