Long March 6

The Long March 6 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) and the Shanghai Academy of Spaceflight Technology (SAST). The rocket was developed in the 2000s, and made its maiden flight in 2015. 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. 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 lb_f) of thrust from burning kerosene and LOX as rocket fuel and oxidiser. This was the first flight of the new engine design.

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2015  Wikimedia, Wikidata
CZ-6; Chang Zheng 6; Changzheng-6; LM-6
diameter 3.35 metre, 
Long March, China National Space Administration, Shanghai Academy of Spaceflight Technology, 
Sweden, Republic of Haiti, 2015, Long March, C, A, Ekran, Dong Fang Hong 2, China National Space Administration, Tarshish, Ashkenaz, Sikh Confederacy, Persia, China, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,

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  Long March 6C ⓘ
  launch vehicle

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  Long March 6A ⓘ
  Chinese launch vehicle

2015-09-19T00:00:00Z

2015-09-19T00:00:00Z

2015 Long March 6

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Frameless

Long March 6 at IAC 2018

Type	Subtype	Date	Description	Notes	Source
class	rocket		Long March 6C	Long March 6	Wikidata
class	rocket	2022	Long March 6A	Long March 6	Wikidata
commons	image		Long March 6 at IAC 2018		Commons