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{{short description|Launch vehicle}} |
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{{Use British English|date=October 2020}} |
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{{Use dmy dates|date=October 2020}} |
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{{Infobox Rocket |
{{Infobox Rocket |
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|name = Long March 6 |
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|image = Maiden Flight of Long March 6 Rocket.jpg |
|image = Maiden Flight of Long March 6 Rocket.jpg |
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|caption = Maiden flight of Long March 6 rocket |
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|function = Small carrier rocket |
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|function = [[Launch vehicle|Small launch vehicle]] |
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|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> |
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|country-origin = [[China]] |
|country-origin = [[China]] |
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|height = {{convert|29|m|ft|abbr=on}} |
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|height = {{cvt|29|m}} |
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|diameter = {{cvt|3.35|m}} |
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|mass = {{cvt|103000|kg}} |
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|stages = 3 <ref name=qq-2013-12-19/> |
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|capacities = {{Infobox Rocket/Payload|location={{convert|700|km|mi|abbr=on}} [[Sun-synchronous orbit|SSO]]|mass={{convert|1080|kg}}}} |
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|family = [[Long March (rocket family)|Long March]]<br/>Long March 6 |
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|capacities = {{Infobox Rocket/Payload |
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|comparable = [[Falcon 1]]<br/>[[Kaituozhe-1]] |
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|location = {{cvt|700|km}} [[Sun-synchronous orbit|SSO]] |
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|status = Active |
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|mass = {{cvt|1080|kg}}}} |
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|sites = LA-16, [[Taiyuan Satellite Launch Center|TSLC]] |
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|launches = 1 |
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|family = [[Long March (rocket family)|Long March]] |
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|success = 1 |
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|comparable = [[Minotaur-C]],<br/>[[PSLV-CA]] |
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|fail = |
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|status = Active |
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|partial = |
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|sites = [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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|first = 19 September 2015<ref>http://news.163.com/15/0920/08/B3UM5LN00001124J.html</ref> |
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|stagedata = |
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|launches = 11 |
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|success = 11 |
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|fail = |
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|partial = |
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|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> |
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|last = 20 June 2023 |
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|stagedata = |
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{{Infobox Rocket/Stage |
{{Infobox Rocket/Stage |
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|type = Stage |
|type = Stage |
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|stageno = First |
|stageno = First |
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|diameter = {{ |
|diameter = {{cvt|3.35|m}} |
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|propmass = {{ |
|propmass = {{cvt|61000|kg}} to {{cvt|76000|kg}} |
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|engines = 1 [[YF-100]] |
|engines = 1 [[YF-100]] |
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|thrust = {{cvt|1188|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/> |
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|thrust = {{convert|1340|kN|lbf|abbr=on}} |
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|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> |
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|burntime = |
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|fuel = [[kerosene|RP-1]]/[[LOX]]}} |
|burntime = |
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|fuel = [[kerosene|RP-1]]/[[LOX]]}} |
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{{Infobox Rocket/Stage |
{{Infobox Rocket/Stage |
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|type = Stage |
|type = Stage |
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|stageno = Second |
|stageno = Second |
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|diameter = {{ |
|diameter = {{cvt|2.25|m}} |
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|propmass = {{ |
|propmass = {{cvt|15000|kg}} |
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|engines = 1 [[YF-115]] |
|engines = 1 [[YF-115]] |
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|thrust = {{cvt|180|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/> |
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|thrust = {{convert|176.5|kN|lbf|abbr=on}} |
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|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> |
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|burntime = |
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|fuel = [[kerosene|RP-1]]/[[LOX]]}} |
|burntime = |
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|fuel = [[kerosene|RP-1]]/[[LOX]]}} |
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{{Infobox Rocket/Stage |
{{Infobox Rocket/Stage |
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|type = Stage |
|type = Stage |
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|stageno = Third |
|stageno = Third |
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|diameter = {{cvt|2.25|m}} |
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|engines =1 |
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|thrust = {{cvt|6.5|kN}} <ref name="New Generation Cryogenic Quick Launching Launch Vehicle and Development"/> |
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|SI = 285 sec |
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|SI = 306.9 seconds |
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|burntime = |
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|fuel = [[Hydrogen Peroxide|H2O2]]/[[kerosene|RP-1]]}} |
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|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" />}} |
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}} |
}} |
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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> |
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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> |
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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/> |
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[[File:Long March 6 on Its Transport Vehicle.jpg|thumb|200px|left|LM-6 on its transport vehicle]] |
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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.<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> |
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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. |
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== Launch statistics == |
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==List of Launches== |
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{{#invoke:Chart | bar chart |
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| height = 300 |
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| width = 500 |
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| stack = 1 |
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| group 1 = 0: 0: 0: 0: 0: 0: 0: 0: 0 |
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| group 2 = 0: 0: 0: 0: 0: 0: 0: 0: 0 |
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| group 3 = 1: 0: 1: 0: 1: 1: 4: 2: 1 |
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| group 4 = 0: 0: 0: 0: 0: 0: 0: 0: 0 |
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| colors = FireBrick : Orange : ForestGreen : LightBlue |
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| group names = Failure : Partial failure : Success : Planned |
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| units suffix = _launches |
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| x legends = 2015 ::::: 2020 ::: |
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}} |
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== List of launches == |
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{{main|List of Long March launches}} |
{{main|List of Long March launches}} |
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{| 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%;"--> |
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|----- style="background:#FFDEAD;" |
|----- style="background:#FFDEAD;" |
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! Flight number |
! Flight number |
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! Serial number |
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! Date (UTC) |
! Date (UTC) |
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! Launch site |
! Launch site |
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Line 65: | Line 98: | ||
! Result |
! Result |
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|- |
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|1 |
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| 1 |
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|September 19, 2015<br />23:01 |
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| Y1 |
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|[[Taiyuan Launch Area 16|LA-16]], [[Taiyuan Satellite Launch Center|TSLC]] |
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| 19 September 2015<br/>23:01 |
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|[[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]] |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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|[[Sun-synchronous orbit|SSO]] |
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| [[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 |
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|{{yes|Success}}<ref name="maidenflight" /> |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}}<ref name="maidenflight"/> |
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|- |
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| 2 |
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| Y2 |
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| 21 November 2017<br/>04:50 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[Jilin 1|Jilin 1-04/05/06]] |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 3 |
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| Y4 |
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| 13 November 2019<br/>06:35 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[Ningxia-1]] 01<br/>[[Ningxia-1]] 02<br/>[[Ningxia-1]] 03<br/>[[Ningxia-1]] 04<br/>[[Ningxia-1]] 05 |
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| [[Low Earth orbit|LEO]] |
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| {{Success}} |
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|- |
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| 4 |
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| Y3 |
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| 6 November 2020<br/>03:19 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[ÑuSat|ÑuSat 9-18]] (10 satellites) |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 5 |
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| Y5 |
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| 27 April 2021<br/>03:20 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| | 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 |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 6 |
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| Y6 |
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| 9 July 2021<br/>11:59 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| Zhuzhou-1 01<br/>Zhuzhou-1 02<br/>Zhuzhou-1 03<br/>Zhuzhou-1 04<br/>Zhuzhou-1 05 |
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| [[Low Earth orbit|LEO]] |
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| {{Success}} |
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|- |
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| 7 |
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| Y7 |
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| 4 August 2021<br/>11:01 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| KL-Beta A<br/>KL-Beta B |
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| [[Polar orbit|Polar]] |
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| {{Success}} |
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|- |
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| 8 |
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| Y8 |
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| 5 November 2021<br/>02:19 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| Guangmu-1 (CASEarth) |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 9 |
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| Y10 |
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| 10 August 2022<br/>04:50 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[Jilin-1|Jilin-1 GF-03D09, 35-43]]<br/>Yunyao-1 04–08<br/>Tianjin Binghai-1 |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 10 |
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| Y9 |
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| 26 September 2022<br/>23:50 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[Shiyan (satellite)|Shiyan 16A]]<br/>[[Shiyan (satellite)|Shiyan 16B]]<br/>[[Shiyan (satellite)|Shiyan 17]] |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 11 |
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| Y12 |
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| 20 June 2023<br/>03:18 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| [[Shiyan (satellite)|Shiyan 25]] |
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| [[Sun-synchronous orbit|SSO]] |
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| {{Success}} |
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|- |
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| 12 |
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| Y? |
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| Q4 2024 |
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| [[Taiyuan Satellite Launch Center|Taiyuan]], [[Taiyuan Launch Area 16|LA-16]] |
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| TBA |
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| TBA |
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| {{Planned}} |
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|} |
|} |
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[[File:Long March 6 at IAC 2018.jpg|thumb|Long March 6 model with launch pad umbilical arm]] |
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==See also== |
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*[[Kaituozhe-1]] |
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== See also == |
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{{Portal|Spaceflight|China}} |
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* [[Comparison of orbital launchers families]] |
* [[Comparison of orbital launchers families]] |
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* [[Comparison of orbital launch systems]] |
* [[Comparison of orbital launch systems]] |
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<!-- These seem unrelated : |
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* {{annotated link|Kaituozhe (rocket family)|Kaituozhe-1}} |
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* {{annotated link|Kuaizhou}} --> |
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== References == |
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{{Reflist|30em|refs= |
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<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> |
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<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> |
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==References== |
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{{reflist|refs= |
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<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> |
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}} |
}} |
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{{Long March rockets}} |
{{Long March rockets}} |
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{{Chinese launch systems}} |
{{Chinese launch systems}} |
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{{Expendable launch systems |
{{Expendable launch systems}} |
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[[Category:Long March (rocket family)]] |
[[Category:Long March (rocket family)]] |
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[[Category: |
[[Category:Spacecraft launched in 2015]] |
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[[Category: |
[[Category:2015 in spaceflight]] |
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[[Category: |
[[Category:2015 in China]] |
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[[Category:Vehicles introduced in 2015]] |
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{{rocketry-stub}} |
![]()
Maiden flight of Long March 6 rocket
| |
Function | Small launch vehicle |
---|---|
Manufacturer | Shanghai Academy of Spaceflight Technology[1] |
Country of origin | China |
Size | |
Height | 29 m (95 ft) |
Diameter | 3.35 m (11.0 ft) |
Mass | 103,000 kg (227,000 lb) |
Stages | 3[2] |
Capacity | |
Payload to 700 km (430 mi) SSO | |
Mass | 1,080 kg (2,380 lb) |
Associated rockets | |
Family | Long March |
Comparable | Minotaur-C, PSLV-CA |
Launch history | |
Status | Active |
Launch sites | Taiyuan, LA-16 |
Total launches | 11 |
Success(es) | 11 |
First flight | 19 September 2015 [3] |
Last flight | 20 June 2023 |
First stage | |
Diameter | 3.35 m (11.0 ft) |
Propellant mass | 61,000 kg (134,000 lb) to 76,000 kg (168,000 lb) |
Powered by | 1YF-100 |
Maximum thrust | 1,188 kN (267,000 lbf) [4] |
Specific impulse | 300 seconds (sea level) 335 seconds (vacuum) [5] |
Propellant | RP-1/LOX |
Second stage | |
Diameter | 2.25 m (7 ft 5 in) |
Propellant mass | 15,000 kg (33,000 lb) |
Powered by | 1YF-115 |
Maximum thrust | 180 kN (40,000 lbf) [4] |
Specific impulse | 341.5 seconds (vacuum) [6] |
Propellant | RP-1/LOX |
Third stage | |
Diameter | 2.25 m (7 ft 5 in) |
Powered by | 1 |
Maximum thrust | 6.5 kN (1,500 lbf) [4] |
Specific impulse | 306.9 seconds |
Propellant | N2O4 / 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]
1
2
3
4
2015
2020
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 |