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- Q11255036 subject Q16269887.
- Q11255036 subject Q7008567.
- Q11255036 subject Q8672072.
- Q11255036 abstract "The YF-100 is a Chinese liquid rocket engine burning LOX and kerosene in an oxidizer-rich staged combustion cycle.Development of the engine began in the 2000s, along with its sibling, the smaller YF-115, which would power the LM-6 and LM-7 upper stages. Testing was directed by the China National Space Administration (CNSA) commencing in 2005. Development works are mainly carried out by the Xi'an Aerospace Propulsion Institute. The engine had its first 300 seconds test fire on November 2007.A high efficiency/high thrust environmentally-friendly rocket engine was always an objective within Programme 863. But Chinese industry was not mature enough to produce such a rocket until they obtained examples (and probably documentation) of the Russian RD-120 in the early 1990.It is the first Chinese rocket engine to adopt the staged-combustion cycle and the most powerful to date. During July 2012 the engine fired for 200 seconds generating 120 t (260,000 lb) of thrust. On May 28, 2012, the National Defense Science and Industry Bureau certified the engine.The engine is planned to be used on the first stage of the Chinese government's next generation of launch vehicles, the Long March 5, the Long March 6 and the Long March 7.".
- Q11255036 wikiPageExternalLink 1532702682.html.
- Q11255036 wikiPageWikiLink Q1090965.
- Q11255036 wikiPageWikiLink Q1161829.
- Q11255036 wikiPageWikiLink Q148.
- Q11255036 wikiPageWikiLink Q16269887.
- Q11255036 wikiPageWikiLink Q201666.
- Q11255036 wikiPageWikiLink Q20936584.
- Q11255036 wikiPageWikiLink Q2668388.
- Q11255036 wikiPageWikiLink Q287464.
- Q11255036 wikiPageWikiLink Q335225.
- Q11255036 wikiPageWikiLink Q3544124.
- Q11255036 wikiPageWikiLink Q519432.
- Q11255036 wikiPageWikiLink Q520336.
- Q11255036 wikiPageWikiLink Q5562673.
- Q11255036 wikiPageWikiLink Q574440.
- Q11255036 wikiPageWikiLink Q618153.
- Q11255036 wikiPageWikiLink Q693470.
- Q11255036 wikiPageWikiLink Q7008567.
- Q11255036 wikiPageWikiLink Q76904.
- Q11255036 wikiPageWikiLink Q787531.
- Q11255036 wikiPageWikiLink Q860308.
- Q11255036 wikiPageWikiLink Q8672072.
- Q11255036 wikiPageWikiLink Q936190.
- Q11255036 comment "The YF-100 is a Chinese liquid rocket engine burning LOX and kerosene in an oxidizer-rich staged combustion cycle.Development of the engine began in the 2000s, along with its sibling, the smaller YF-115, which would power the LM-6 and LM-7 upper stages. Testing was directed by the China National Space Administration (CNSA) commencing in 2005. Development works are mainly carried out by the Xi'an Aerospace Propulsion Institute.".
- Q11255036 label "YF-100".