Editing Chinese space program (section)

===Launch vehicles===

==== Active or under development ====
* [[Air-Launched SLV]] able to place a 50 kilogram plus payload to 500&nbsp;km [[Sun-synchronous orbit|SSO]]<ref>{{cite web|url=http://news.xinhuanet.com/mil/2006-11/01/content_5274571.htm|title=空射运载火箭亮相珠海航展|publisher=[[新华网]]|date=2006-11-01|access-date=May 3, 2008|url-status=dead|archive-url=https://web.archive.org/web/20080207113726/http://news.xinhuanet.com/mil/2006-11/01/content_5274571.htm|archive-date=February 7, 2008}}</ref>
* [[Galactic Energy|Ceres-1]] small-lift solid-fueled launch vehicle from private firm (relatively high launch cadence)
* [[Orienspace|Gravity-1]] medium-lift sea-launched solid fuel launch vehicle under development 
* [[i-Space (Chinese company)#Hyperbola-1|Hyperbola-1]] small-lift solid-fueled launch vehicle from private firm
* [[i-Space (Chinese company)|Hyperbola-3]] medium-lift liquid-fueled (methalox) launch vehicle with reusable first stage (VTVL) from private firm currently under development
* [[Jielong 3]] small to medium-lift solid fueled launch vehicle currently in service
*[[Kaituozhe (rocket family)#Kaituozhe-1|Kaituozhe-1A]] ({{Zh|labels=no|s=开拓者一号甲}})
* [[Kuaizhou]] quick-reaction small-lift solid fuel launch vehicle
* [[CAS Space|Lijian-1]] small to medium-lift solid fuel launch vehicle currently in service (by the commercial spin-off of the [[Chinese Academy of Sciences]])
* [[CAS Space|Lijian-2]] medium-lift launch vehicle utilizing liquid fuel (kerolox) with reusable first stage under development
* [[Long March 2 rocket family|CZ-2E(A)]] Intended for launch of Chinese space station modules. Payload capacity up to 14 tons in LEO and 9000 (kN) liftoff thrust developed by 12 rocket engines, with enlarged fairing of 5.20 m in diameter and length of 12.39 m to accommodate large spacecraft<ref>{{cite web |url=http://www.cardc.cn/show_field.asp?wt_id=2&field_name=WT_PROJECT |title=CZ-2EA地面风载试验 |publisher=[[中国空气动力研究与发展中心]] |date=2008-02-04 |access-date=June 30, 2008 |url-status=dead |archive-url=https://web.archive.org/web/20090213163801/http://www.cardc.cn/show_field.asp?wt_id=2&field_name=WT_PROJECT |archive-date=February 13, 2009 }}</ref>
* [[Long March 2 rocket family|CZ-2F/G]] Modified [[CZ-2F]] without escape tower, specially used for launching robotic missions such as Shenzhou cargo and space laboratory module with payload capacity up to 11.2 tons in LEO<ref>{{cite web|url=http://scitech.people.com.cn/GB/7425999.html|title=独家："神八"将用改进型火箭发射 2010年左右首飞|publisher=人民网|date=June 25, 2008|access-date=June 26, 2008|archive-date=June 10, 2016|archive-url=https://web.archive.org/web/20160610101726/http://scitech.people.com.cn/GB/7425999.html|url-status=dead}}</ref>
* [[Long March 3 rocket family|CZ-3B(A)]] More powerful Long March rockets using larger-size liquid propellant strap-on motors, with payload capacity up to 13 tons in LEO
* [[Long March 3C|CZ-3C]] Launch vehicle combining [[Long March 3 rocket family|CZ-3B]] core with two boosters from [[Long March 2 rocket family|CZ-2E]]
* [[Long March 4C]]
* [[Long March 5 rocket family|CZ-5]] heavy-lift hydrolox launch vehicle (with kerolox boosters)
* [[Long March 5|CZ-5B]] variant of the CZ-5 for low Earth orbit payloads (up to 25 tonnes to [[low Earth orbit|LEO]])
* [[Chang Zheng 6|CZ-6]] or Small Launch Vehicle; small-lift kerolox LV with short launch preparation period, low cost and high reliability, to meet the launch need of small satellites up to 500&nbsp;kg to 700&nbsp;km [[Sun synchronous orbit|SSO]], first flight for 2010; with [[Fan Ruixiang]] ({{Zh|labels=no|s=范瑞祥}}) as Chief designer of the project<ref>{{cite web|url=http://www.rensb.com/showarticle.php?articleID=9325 |archive-url=https://web.archive.org/web/20110715172931/http://www.rensb.com/showarticle.php?articleID=9325 |url-status=dead |archive-date=2011-07-15 |title=让年轻人与航天事业共同成长 |publisher=中国人事报 |date=2008-03-14 |access-date=July 19, 2008 }}</ref><ref>{{cite book|author=中国科学技术协会|year=2007|title=航天科学技术学科发展报告|page=17|url=http://mallimg.sina.com.cn/p/bookuu/001/704/PD_1704953L.jpg|archive-url=https://web.archive.org/web/20080911054009/http://mallimg.sina.com.cn/p/bookuu/001/704/PD_1704953L.jpg|url-status=dead|archive-date=2008-09-11|publisher=中国科学技术协会出版社|location=[[Beijing]], PRC|isbn=978-7504648662}}</ref><ref>{{cite web|url=http://news.people.com.cn/GB/5971395.html|title=国际空间大学公众论坛关注中国航天（3）|publisher=[[People Daily]]|date=2007-07-11|access-date=July 13, 2007|archive-url=https://web.archive.org/web/20160303182108/http://news.people.com.cn/GB/5971395.html|archive-date=March 3, 2016|url-status=dead}}</ref>
* [[Chang Zheng 7|CZ-7]] medium-lift kerolox launch vehicle for launching resupply missions to the [[Tiangong space station]]
* [[Long March 8|CZ-8]] medium-lift launch vehicle mainly for launching payloads to [[Sun-synchronous orbit|SSO]] orbits
* [[Long March 9|CZ-9]] super heavy-lift launch vehicle with a LEO lift capability of 150 tonnes currently under development (planned to be fully reusable in time)
* [[Long March 10|CZ-10]] crew-rated super-heavy launch vehicle for crewed lunar missions under development
* [[Long March 10|CZ-10A]] crew-rated medium-lift launch vehicle for launching the [[next-generation crewed spacecraft]] to [[low Earth orbit|LEO]]s  with reusable first stage currently under development
* [[Long March 11|CZ-11]] small-lift solid fuel quick-response launch vehicle
* [[Pallas-1]] reusable (1st stage) medium-lift liquid fuel (kerolox) launch vehicle by private firm currently under development
* [[Project 921-3#Reusable launch vehicle|Project 921-3 Reusable launch vehicle]] current project of the reusable shuttle system.
* [[Project 921-3#Tengyun|Tengyun]] another current project of two wing-staged reusable shuttle system
* [[Chinese reusable experimental spacecraft|Reusable spaceplane]] reusable vertically-launched spaceplane with wings that lands on a runway and currently in service (speculated to be similar to the US [[X-37|X-37B]] in form and function)
* [[Space Pioneer#Rockets|Tianlong 2]] medium-lift kerolox launch vehicle from private firm (in service)
* [[Space Pioneer#Rockets|Tianlong 3]] medium to heavy-lift kerolox launch vehicle with reusable first stage from private firm currently under development
* [[Zhuque-2]] medium-lift liquid fuel (methalox) launch vehicle by private firm currently in service (first methane fueled rocket in the world to reach space and to reach orbit with payload)
* [[LandSpace Technology Corporation#Zhuque-3|Zhuque-3]] medium to heavy-lift methalox launch vehicle by private firm with reusable first stage currently under development

==== Cancelled/retired ====

* [[Long March 1 rocket family|CZ-1D]] based on a [[Long March 1 rocket family|CZ-1]] but with a new N<sub>2</sub>O<sub>4</sub>/UDMH second stage.
* [[Project 921-3#869 Project|Project 869]] reusable shuttle system with Tianjiao-1 or Chang Cheng-1 (Great Wall-1) orbiters. Project of 1980s-1990s.