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1 Launch statistics  





2 List of launches  





3 See also  





4 References  














Long March 6: Difference between revisions






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Line 1: Line 1:

{{short description|Launch vehicle}}

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

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

{{Infobox Rocket

{{Infobox Rocket

|name = Long March 6

|image = Maiden Flight of Long March 6 Rocket.jpg

|image = Maiden Flight of Long March 6 Rocket.jpg

|image caption = Maiden flight of Long March 6 rocket

|caption = Maiden flight of Long March 6 rocket


|function = Small carrier rocket

|manufacturer = [[China Academy of Launch Vehicle Technology|CALT]]

|function = [[Launch vehicle|Small launch vehicle]]

|manufacturer = [[Shanghai Academy of Spaceflight Technology]]<ref name=nasaspaceflight>{{cite web|url=http://www.nasaspaceflight.com/2015/09/china-debut-launch-long-march-6/|title=China conducts debut launch of Long March 6|date=19 September 2015 |publisher=NASASpaceflight|access-date=2015-09-19}}</ref>

|country-origin = [[China]]

|country-origin = [[China]]


|height = {{convert|29|m|ft|abbr=on}}

|diameter = {{convert|3.35|m|ft|abbr=on}}

|height = {{cvt|29|m}}

|mass = {{convert|103000|kg|lbs|abbr=on}}

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

|stages = 3<ref name=qq-2013-12-19 />

|mass = {{cvt|103000|kg}}

|stages = 3 <ref name=qq-2013-12-19/>

|capacities = {{Infobox Rocket/Payload|location={{convert|700|km|mi|abbr=on}} [[Sun-synchronous orbit|SSO]]|mass={{convert|1080|kg}}}}


|family = [[Long March (rocket family)|Long March]]<br/>Long March 6

|capacities = {{Infobox Rocket/Payload

|comparable = [[Falcon 1]]<br/>[[Kaituozhe-1]]

|location = {{cvt|700|km}} [[Sun-synchronous orbit|SSO]]

|status = Active

|mass = {{cvt|1080|kg}}}}

|sites = LA-16, [[Taiyuan Satellite Launch Center|TSLC]]


|launches = 1

|family = [[Long March (rocket family)|Long March]]

|success = 1

|comparable = [[Minotaur-C]],<br/>[[PSLV-CA]]

|fail =

|status = Active

|partial =

|sites = [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

|first = 19 September 2015<ref>http://news.163.com/15/0920/08/B3UM5LN00001124J.html</ref>


|stagedata =

|launches = 11

|success = 11

|fail =

|partial =

|first = 19 September 2015 <ref name=News163-20-star>[http://news.163.com/15/0920/08/B3UM5LN00001124J.html ''The Long March 6 launched a 20-star in Taiyuan to create the best in Asia'' Sept 2015]</ref>

|last = 20 June 2023


|stagedata =

{{Infobox Rocket/Stage

{{Infobox Rocket/Stage

|type = Stage

|type = Stage

|stageno = First

|stageno = First

|diameter = {{convert|3.35|m|ft|abbr=on}}

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

|propmass = {{convert|61000|kg|lbs|abbr=on}} to {{convert|76000|kg|lbs|abbr=on}}

|propmass = {{cvt|61000|kg}} to {{cvt|76000|kg}}

|engines = 1 [[YF-100]]

|engines = 1 [[YF-100]]

|thrust = {{cvt|1188|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/>

|thrust = {{convert|1340|kN|lbf|abbr=on}}

|SI = 300 seconds ([[sea level]])<br/>335 seconds ([[vacuum]]) <ref name=spacepac>{{cite web|url=http://spacepac.org/wp/china/chinese-yf-100-russian-rd-120-to-power-cz-5|title=Chinese YF-100 (Russian RD-120) to Power CZ-5|publisher=SPACEPAC, The Space Public Affairs Committee|access-date=2015-07-02|archive-date=25 October 2017|archive-url=https://web.archive.org/web/20171025141442/http://spacepac.org/wp/china/chinese-yf-100-russian-rd-120-to-power-cz-5/|url-status=dead}}</ref>

|burntime =

|fuel = [[kerosene|RP-1]]/[[LOX]]}}

|burntime =

|fuel = [[kerosene|RP-1]]/[[LOX]]}}


{{Infobox Rocket/Stage

{{Infobox Rocket/Stage

|type = Stage

|type = Stage

|stageno = Second

|stageno = Second

|diameter = {{convert|2.25|m|ft|abbr=on}}

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

|propmass = {{convert|15000|kg|lbs|abbr=on}}

|propmass = {{cvt|15000|kg}}

|engines = 1 [[YF-115]]

|engines = 1 [[YF-115]]

|thrust = {{cvt|180|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/>

|thrust = {{convert|176.5|kN|lbf|abbr=on}}

|SI = 341.5 seconds (vacuum) <ref name=shenkongnet>{{cite web|url=http://www.shenkong.net/Explore/1410/ZGXYDYYMYFDJ3-YF100-115ZYTX26045110.htm|title=中国新一代液氧煤油发动机3:YF100/115主要特性 - 深空网 |website=www.shenkong.net|language=Chinese|access-date=2016-04-11|url-status=dead|archiveurl=https://web.archive.org/web/20160304055915/http://www.shenkong.net/Explore/1410/ZGXYDYYMYFDJ3-YF100-115ZYTX26045110.htm|archive-date=2016-03-04}}</ref>

|burntime =

|fuel = [[kerosene|RP-1]]/[[LOX]]}}

|burntime =

|fuel = [[kerosene|RP-1]]/[[LOX]]}}


{{Infobox Rocket/Stage

{{Infobox Rocket/Stage

|type = Stage

|type = Stage

|stageno = Third

|stageno = Third

|engines = 4 [[YF-85]]

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

|thrust = {{convert|4|kN|lbf|abbr=on}}

|engines =1

|thrust = {{cvt|6.5|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/>

|SI = 285 sec

|burntime =

|SI = 306.9 seconds

|burntime =

|fuel = [[Hydrogen Peroxide|H2O2]]/[[kerosene|RP-1]]}}

|fuel = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[Unsymmetrical dimethylhydrazine|UDMH]]<ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development" />}}

}}

}}

The '''Long March 6''' ({{zh|c=长征六号运载火箭}}) or '''Chang Zheng 6''' as in [[pinyin]], abbreviated '''LM-6''' for export or '''CZ-6''' within China, is a [[China|Chinese]] [[liquid-fuel rocket|liquid-fuelled]] [[launch vehicle|carrier rocket]], which was developed by the [[China Aerospace Science and Technology Corporation]]<ref>{{cite web|url=http://english.people.com.cn/90001/90776/90881/6748699.html|title=Development of China's new "Changzheng 6" carrier rocket commences|publisher=People's Daily Online|date=2009-09-04|accessdate=2009-09-06}}</ref> and the [[China Academy of Launch Vehicle Technology]], and made its maiden flight in 2015.<ref name="maidenflight">{{cite web|url=http://www.nasaspaceflight.com/2015/09/china-debut-launch-long-march-6/ |title=China conducts debut launch of Long March 6|date=2015-09-19|accessdate=2015-09-20}}</ref>

As one of the new generation rocket family, the Long March 6 was designed to be a light capacity, "high-speed response" rocket, complementing the heavy lift [[Long March 5]] and the mid-heavy lift [[Long March 7]] rocket families. It is capable of placing at least {{convert|1000|kg}} of payload into a [[sun-synchronous orbit]].<ref>http://www.spaceflight101.com/long-march-6.html</ref><ref name="SD">{{cite web|url=http://www.nasaspaceflight.com/2015/09/china-debut-launch-long-march-6/|title=China conducts debut launch of Long March 6|publisher=nasaspaceflight.com}}</ref>



The '''Long March 6''' ({{zh|c=长征六号运载火箭}}) or '''Chang Zheng 6''' as in [[pinyin]], abbreviated '''LM 6''' for export or '''CZ 6''' within China, is a Chinese [[liquid-fuel rocket|liquid-fuelled]] [[launch vehicle]] of the [[Long March (rocket family)|Long March family]], which was developed by the [[China Aerospace Science and Technology Corporation]] (CASC) <ref>{{cite web |url=http://english.people.com.cn/90001/90776/90881/6748699.html|title=Development of China's new "Changzheng 6" carrier rocket commences|publisher=People's Daily Online|date=2009-09-04|access-date=6 September 2009}}</ref> and the [[Shanghai Academy of Spaceflight Technology]] (SAST). The rocket was developed in the 2000s, and made its maiden flight in 2015.<ref name="maidenflight">{{cite web |url=http://www.nasaspaceflight.com/2015/09/china-debut-launch-long-march-6/|title=China conducts debut launch of Long March 6|date=2015-09-19|access-date=20 September 2015}}</ref> As one of the new generation rocket family, the Long March 6 was designed to be a light capacity, "high-speed response" rocket, complementing the heavy lift [[Long March 5]] and the mid-heavy lift [[Long March 7]] rocket families. It is capable of placing at least {{cvt|1000|kg}} of payload into a [[Sun-synchronous orbit]].<ref>{{cite web|url=http://www.spaceflight101.com/long-march-6.html|title=Long March 6 - Spaceflight101|access-date=2015-09-20|url-status=dead|archiveurl=https://archive.today/20150918112832/http://www.spaceflight101.com/long-march-6.html|archive-date=18 September 2015}}</ref><ref name="maidenflight"/> The first stage of the Long March 6 was derived from the [[booster rocket]]s being developed for the [[Long March 5]] rocket. It is powered by a [[YF-100]] engine, which generates {{cvt|1340|kN}} of thrust from burning [[kerosene]] and [[LOX]] as [[rocket fuel]] and [[oxidiser]].<ref name="maidenflight"/> This was the first flight of the new engine design.<ref name=News163-20-star/>

[[File:Long March 6 on Its Transport Vehicle.jpg|thumb|200px|left|LM-6 on its transport vehicle]]



An enlarged variant, the [[Long March 6A]], which has four strap-on solid boosters, an elongated stage one, a new stage two with the same diameter as the first stage, and a payload capacity of at least 4000&nbsp;kg to [[Sun-synchronous orbit]], made its maiden flight on 29 March 2022.<ref>{{cite web|url=http://space.skyrocket.de/doc_lau/cz-6.htm|title=CZ-6 (Chang Zheng-6)|website=space.skyrocket.de|access-date=2 November 2017}}</ref> A further iteration named the [[Long March 6C]] with a slightly shorter length than the 6A and without the four strap-on solid boosters had its successful maiden launch on 7 May 2024.<ref name=AJ-CZ6C>{{cite web | url=https://spacenews.com/china-launches-first-long-march-6c-rocket/ | last=Jones | first=Andrew | title=China launches first Long March 6C rocket | publisher=spacenews.com | date=7 May 2024 | access-date=7 May 2024}}</ref>

The first stage of the Long March 6 was derived from the [[booster rocket]]s being developed for the [[Long March 5]] rocket. It is powered by a [[YF-100]] engine, which generates {{convert|1340|kN|disp=or}} of thrust from burning [[kerosene]] and [[LOX]] as [[rocket fuel]] and [[oxidiser]].<ref name="SD"/>The maiden flight was expected to take place on 18 September 2015, but was delayed and occurred on 19 September at 23:01:14 UTC.



== Launch statistics ==

==List of Launches==

{{#invoke:Chart | bar chart

| height = 300

| width = 500

| stack = 1

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

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

| group 3 = 1: 0: 1: 0: 1: 1: 4: 2: 1

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


| colors = FireBrick : Orange : ForestGreen : LightBlue

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

| units suffix = _launches

| x legends = 2015 ::::: 2020 :::

}}


== List of launches ==

{{main|List of Long March launches}}

{{main|List of Long March launches}}

{| class="wikitable" <!--border="2" cellpadding="4" cellspacing="0" style="margin: 0.5em 0em 0.5em 0; background: #f9f9f9; border: 1px #aaa solid; border-collapse: collapse; font-size: 95%;"-->

{| class="wikitable" <!--border="2" cellpadding="4" cellspacing="0" style="margin: 0.5em 0em 0.5em 0; background: #f9f9f9; border: 1px #aaa solid; border-collapse: collapse; font-size: 95%;"-->

|----- style="background:#FFDEAD;"

|----- style="background:#FFDEAD;"

! Flight number

! Flight number

! Serial number

! Date (UTC)

! Date (UTC)

! Launch site

! Launch site

Line 65: Line 98:

! Result

! Result

|-

|-


|1

| 1

|September 19, 2015<br />23:01

| Y1

|[[Taiyuan Launch Area 16|LA-16]], [[Taiyuan Satellite Launch Center|TSLC]]

| 19 September 2015<br/>23:01

|[[ZDPS-2A]]<br>[[ZDPS-2B]]<br>[[NanoSatellite-2|NS-2]]<br>[[Zijing-1|ZJ-1]]<br>[[Zijing-2|ZJ-2]]<br>[[Tiantuo 3]]<br>[[NUDT-Phone-Sat]]<br>[[Xingchen 1]]<br>[[Xingchen 2]]<br>[[Xingchen 3]]<br>[[Xingchen 4]]<br>[[LilacSat 2]]<br>[[Xinyan-2|XY-2]]<br>DCBB<br>[[Xiwang-2A]]<br>[[Xiwang-2B]]<br>[[Xiwang-2C]]<br>[[Xiwang-2D]]<br>[[Xiwang-2E]]<br>[[Xiwang-2F]]

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

|[[Sun-synchronous orbit|SSO]]

| [[ZDPS-2A]], [[ZDPS-2B]]<br>[[NanoSatellite-2|NS-2]]<br>[[Zijing-1|ZJ-1]], [[Zijing-2|ZJ-2]]<br>[[Tiantuo 3]]<br>[[NUDT-Phone-Sat]]<br>[[Xingchen]] 1/2/3/4<br>[[LilacSat 2]]<br>[[Xinyan-2|XY-2]]<br>[[DCBB]]<br>[[Xiwang]]-2A/2B/2C/2E/2F

|{{yes|Success}}<ref name="maidenflight" />

| [[Sun-synchronous orbit|SSO]]

| {{Success}}<ref name="maidenflight"/>

|-


| 2

| Y2

| 21 November 2017<br/>04:50

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[Jilin 1|Jilin 1-04/05/06]]

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 3

| Y4

| 13 November 2019<br/>06:35

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[Ningxia-1]] 01<br/>[[Ningxia-1]] 02<br/>[[Ningxia-1]] 03<br/>[[Ningxia-1]] 04<br/>[[Ningxia-1]] 05

| [[Low Earth orbit|LEO]]

| {{Success}}

|-


| 4

| Y3

| 6 November 2020<br/>03:19

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[ÑuSat|ÑuSat 9-18]] (10 satellites)

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 5

| Y5

| 27 April 2021<br/>03:20

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| | Qilu-1<br/>Qilu-4<br/>Foshan-1<br/>Zhongan Guotong-1<br/>Tianqi-9<br/>Origin Space NEO-1<br/>Tai King II 01<br/>Golden Bauhinia-1 01<br/>Golden Bauhinia-1 02

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 6

| Y6

| 9 July 2021<br/>11:59

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| Zhuzhou-1 01<br/>Zhuzhou-1 02<br/>Zhuzhou-1 03<br/>Zhuzhou-1 04<br/>Zhuzhou-1 05

| [[Low Earth orbit|LEO]]

| {{Success}}

|-


| 7

| Y7

| 4 August 2021<br/>11:01

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| KL-Beta A<br/>KL-Beta B

| [[Polar orbit|Polar]]

| {{Success}}

|-


| 8

| Y8

| 5 November 2021<br/>02:19

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| Guangmu-1 (CASEarth)

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 9

| Y10

| 10 August 2022<br/>04:50

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[Jilin-1|Jilin-1 GF-03D09, 35-43]]<br/>Yunyao-1 04–08<br/>Tianjin Binghai-1

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 10

| Y9

| 26 September 2022<br/>23:50

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[Shiyan (satellite)|Shiyan 16A]]<br/>[[Shiyan (satellite)|Shiyan 16B]]<br/>[[Shiyan (satellite)|Shiyan 17]]

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 11

| Y12

| 20 June 2023<br/>03:18

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| [[Shiyan (satellite)|Shiyan 25]]

| [[Sun-synchronous orbit|SSO]]

| {{Success}}

|-


| 12

| Y?

| Q4 2024

| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]]

| TBA

| TBA

| {{Planned}}

|}

|}



[[File:Long March 6 at IAC 2018.jpg|thumb|Long March 6 model with launch pad umbilical arm]]

==See also==


*[[Kaituozhe-1]]

== See also ==

{{Portal|Spaceflight|China}}

* [[Comparison of orbital launchers families]]

* [[Comparison of orbital launchers families]]

* [[Comparison of orbital launch systems]]

* [[Comparison of orbital launch systems]]

<!-- These seem unrelated :

* {{annotated link|Kaituozhe (rocket family)|Kaituozhe-1}}

* {{annotated link|Kuaizhou}} -->


== References ==

{{Reflist|30em|refs=


<ref name=qq-2013-12-19>{{cite web|url=http://news.qq.com/a/20131219/013441_all.htm|title=突破运力"下限"的长征6号|trans-title=Advances in Light Capacity Long March 6|publisher=Tencent Military Channel |language=Chinese|date=19 December 2013|access-date=3 August 2015}}</ref>



<ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development">{{cite journal|author=ZHANG Wei-dong, WANG Dong-bao|title=New Generation Cryogenic Quick Launching Launch Vehicle and Development|journal=Aerospace Shanghai|date=2016}}</ref>

==References==

{{reflist|refs=

<ref name=qq-2013-12-19>{{cite web |url=http://news.qq.com/a/20131219/013441_all.htm |title=突破运力“下限”的长征6号 |trans-title=Advances in Light Capacity Long March 6 |publisher=Tencent Military Channel |accessdate=2015-08-03 |language=Chinese |date=2013-12-19}}</ref>

}}

}}



{{Long March rockets}}

{{Long March rockets}}

{{Chinese launch systems}}

{{Chinese launch systems}}

{{Expendable launch systems|state=expanded}}

{{Expendable launch systems}}



[[Category:Long March (rocket family)]]

[[Category:Long March (rocket family)]]

[[Category:2013 introductions]]

[[Category:Spacecraft launched in 2015]]

[[Category:2013 in spaceflight]]

[[Category:2015 in spaceflight]]

[[Category:2013 in China]]

[[Category:2015 in China]]

[[Category:Vehicles introduced in 2015]]



{{rocketry-stub}}


Latest revision as of 16:22, 22 June 2024

Long March 6
Maiden flight of Long March 6 rocket
FunctionSmall launch vehicle
ManufacturerShanghai Academy of Spaceflight Technology[1]
Country of originChina
Size
Height29 m (95 ft)
Diameter3.35 m (11.0 ft)
Mass103,000 kg (227,000 lb)
Stages3[2]
Capacity
Payload to 700 km (430 mi) SSO
Mass1,080 kg (2,380 lb)
Associated rockets
FamilyLong March
ComparableMinotaur-C,
PSLV-CA
Launch history
StatusActive
Launch sitesTaiyuan, LA-16
Total launches11
Success(es)11
First flight19 September 2015 [3]
Last flight20 June 2023
First stage
Diameter3.35 m (11.0 ft)
Propellant mass61,000 kg (134,000 lb) to 76,000 kg (168,000 lb)
Powered by1YF-100
Maximum thrust1,188 kN (267,000 lbf) [4]
Specific impulse300 seconds (sea level)
335 seconds (vacuum) [5]
PropellantRP-1/LOX
Second stage
Diameter2.25 m (7 ft 5 in)
Propellant mass15,000 kg (33,000 lb)
Powered by1YF-115
Maximum thrust180 kN (40,000 lbf) [4]
Specific impulse341.5 seconds (vacuum) [6]
PropellantRP-1/LOX
Third stage
Diameter2.25 m (7 ft 5 in)
Powered by1
Maximum thrust6.5 kN (1,500 lbf) [4]
Specific impulse306.9 seconds
PropellantN2O4 / UDMH[4]

The Long March 6 (Chinese: 长征六号运载火箭) or Chang Zheng 6 as in pinyin, abbreviated LM 6 for export or CZ 6 within China, is a Chinese liquid-fuelled launch vehicle of the Long March family, which was developed by the China Aerospace Science and Technology Corporation (CASC) [7] and the Shanghai Academy of Spaceflight Technology (SAST). The rocket was developed in the 2000s, and made its maiden flight in 2015.[8] As one of the new generation rocket family, the Long March 6 was designed to be a light capacity, "high-speed response" rocket, complementing the heavy lift Long March 5 and the mid-heavy lift Long March 7 rocket families. It is capable of placing at least 1,000 kg (2,200 lb) of payload into a Sun-synchronous orbit.[9][8] The first stage of the Long March 6 was derived from the booster rockets being developed for the Long March 5 rocket. It is powered by a YF-100 engine, which generates 1,340 kN (300,000 lbf) of thrust from burning kerosene and LOXasrocket fuel and oxidiser.[8] This was the first flight of the new engine design.[3]

An enlarged variant, the Long March 6A, which has four strap-on solid boosters, an elongated stage one, a new stage two with the same diameter as the first stage, and a payload capacity of at least 4000 kg to Sun-synchronous orbit, made its maiden flight on 29 March 2022.[10] A further iteration named the Long March 6C with a slightly shorter length than the 6A and without the four strap-on solid boosters had its successful maiden launch on 7 May 2024.[11]

Launch statistics[edit]

1

2

3

4

2015

2020

List of launches[edit]

Flight number Serial number Date (UTC) Launch site Payload Orbit Result
1 Y1 19 September 2015
23:01
Taiyuan, LA-16 ZDPS-2A, ZDPS-2B
NS-2
ZJ-1, ZJ-2
Tiantuo 3
NUDT-Phone-Sat
Xingchen 1/2/3/4
LilacSat 2
XY-2
DCBB
Xiwang-2A/2B/2C/2E/2F
SSO Success[8]
2 Y2 21 November 2017
04:50
Taiyuan, LA-16 Jilin 1-04/05/06 SSO Success
3 Y4 13 November 2019
06:35
Taiyuan, LA-16 Ningxia-101
Ningxia-102
Ningxia-103
Ningxia-104
Ningxia-105
LEO Success
4 Y3 6 November 2020
03:19
Taiyuan, LA-16 ÑuSat 9-18 (10 satellites) SSO Success
5 Y5 27 April 2021
03:20
Taiyuan, LA-16 Qilu-1
Qilu-4
Foshan-1
Zhongan Guotong-1
Tianqi-9
Origin Space NEO-1
Tai King II 01
Golden Bauhinia-1 01
Golden Bauhinia-1 02
SSO Success
6 Y6 9 July 2021
11:59
Taiyuan, LA-16 Zhuzhou-1 01
Zhuzhou-1 02
Zhuzhou-1 03
Zhuzhou-1 04
Zhuzhou-1 05
LEO Success
7 Y7 4 August 2021
11:01
Taiyuan, LA-16 KL-Beta A
KL-Beta B
Polar Success
8 Y8 5 November 2021
02:19
Taiyuan, LA-16 Guangmu-1 (CASEarth) SSO Success
9 Y10 10 August 2022
04:50
Taiyuan, LA-16 Jilin-1 GF-03D09, 35-43
Yunyao-1 04–08
Tianjin Binghai-1
SSO Success
10 Y9 26 September 2022
23:50
Taiyuan, LA-16 Shiyan 16A
Shiyan 16B
Shiyan 17
SSO Success
11 Y12 20 June 2023
03:18
Taiyuan, LA-16 Shiyan 25 SSO Success
12 Y? Q4 2024 Taiyuan, LA-16 TBA TBA Planned
Long March 6 model with launch pad umbilical arm

See also[edit]

References[edit]

  1. ^ "China conducts debut launch of Long March 6". NASASpaceflight. 19 September 2015. Retrieved 19 September 2015.
  • ^ "突破运力"下限"的长征6号" [Advances in Light Capacity Long March 6] (in Chinese). Tencent Military Channel. 19 December 2013. Retrieved 3 August 2015.
  • ^ a b The Long March 6 launched a 20-star in Taiyuan to create the best in Asia Sept 2015
  • ^ a b c d ZHANG Wei-dong, WANG Dong-bao (2016). "New Generation Cryogenic Quick Launching Launch Vehicle and Development". Aerospace Shanghai.
  • ^ "Chinese YF-100 (Russian RD-120) to Power CZ-5". SPACEPAC, The Space Public Affairs Committee. Archived from the original on 25 October 2017. Retrieved 2 July 2015.
  • ^ "中国新一代液氧煤油发动机3:YF100/115主要特性 - 深空网". www.shenkong.net (in Chinese). Archived from the original on 4 March 2016. Retrieved 11 April 2016.
  • ^ "Development of China's new "Changzheng 6" carrier rocket commences". People's Daily Online. 4 September 2009. Retrieved 6 September 2009.
  • ^ a b c d "China conducts debut launch of Long March 6". 19 September 2015. Retrieved 20 September 2015.
  • ^ "Long March 6 - Spaceflight101". Archived from the original on 18 September 2015. Retrieved 20 September 2015.
  • ^ "CZ-6 (Chang Zheng-6)". space.skyrocket.de. Retrieved 2 November 2017.
  • ^ Jones, Andrew (7 May 2024). "China launches first Long March 6C rocket". spacenews.com. Retrieved 7 May 2024.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Long_March_6&oldid=1230420285"

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