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- YF-115 abstract "The YF-115 is a Chinese liquid rocket engine burning LOX and kerosene in an oxidizer-rich staged combustion cycle. A high efficiency/high thrust environmental friendly rocket engine was always an objective within Programme 863. But the 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. Development began in the 2000s, along with its sibling, the bigger YF-100, which would power the LM-5, LM-6 and LM-7 boosters and first 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. It will be used as upper stage engine for China's next generation of medium and light environmental-friendly launch vehicles, namely the Long March 6 and the Long March 7. During early 2012, the engine system successfully passed vacuum testing. It is China's first upper stage rocket engine to adopt the staged-combustion cycle.In the LM-6 upper stage it will use a single YF-115 with gimbaled mount. While the LM-7 upper stage will use four such engines. But in this latter case, two engines will be fixed and two will be gimbaled.".
- YF-115 wikiPageID "47144145".
- YF-115 wikiPageLength "5540".
- YF-115 wikiPageOutDegree "29".
- YF-115 wikiPageRevisionID "698158348".
- YF-115 wikiPageWikiLink 863_Program.
- YF-115 wikiPageWikiLink Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-115 wikiPageWikiLink Category:Rocket_engines.
- YF-115 wikiPageWikiLink Category:Rocket_engines_of_China.
- YF-115 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- YF-115 wikiPageWikiLink China.
- YF-115 wikiPageWikiLink Gimbaled_thrust.
- YF-115 wikiPageWikiLink Government_of_China.
- YF-115 wikiPageWikiLink Kerosene.
- YF-115 wikiPageWikiLink Liquid-propellant_rocket.
- YF-115 wikiPageWikiLink Liquid_oxygen.
- YF-115 wikiPageWikiLink Long_March_5.
- YF-115 wikiPageWikiLink Long_March_6.
- YF-115 wikiPageWikiLink Long_March_7.
- YF-115 wikiPageWikiLink RD-120.
- YF-115 wikiPageWikiLink RP-1.
- YF-115 wikiPageWikiLink Rocket_engine.
- YF-115 wikiPageWikiLink Staged_combustion_cycle.
- YF-115 wikiPageWikiLink YF-100.
- YF-115 wikiPageWikiLinkText "YF-115".
- YF-115 associated "--03-06".
- YF-115 combustionChamber "1".
- YF-115 countryOfOrigin China.
- YF-115 cycle "Oxidizer-rich Staged combustion".
- YF-115 designer Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-115 firstDate "2015-09-20".
- YF-115 fuel RP-1.
- YF-115 mixtureRatio "2.5".
- YF-115 name "YF-115".
- YF-115 oxidiser Liquid_oxygen.
- YF-115 status "In service".
- YF-115 type "liquid".
- YF-115 usedIn "7.0".
- YF-115 wikiPageUsesTemplate Template:Convert.
- YF-115 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- YF-115 wikiPageUsesTemplate Template:Reflist.
- YF-115 wikiPageUsesTemplate Template:Rocket-stub.
- YF-115 wikiPageUsesTemplate Template:Rocket_Engines.
- YF-115 subject Category:Rocket_engines.
- YF-115 subject Category:Rocket_engines_of_China.
- YF-115 subject Category:Rocket_engines_using_kerosene_propellant.
- YF-115 hypernym LOX.
- YF-115 comment "The YF-115 is a Chinese liquid rocket engine burning LOX and kerosene in an oxidizer-rich staged combustion cycle. A high efficiency/high thrust environmental friendly rocket engine was always an objective within Programme 863. But the 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.".
- YF-115 label "YF-115".
- YF-115 sameAs Q20936584.
- YF-115 sameAs YF-115.
- YF-115 sameAs YF-115.
- YF-115 sameAs Q20936584.
- YF-115 wasDerivedFrom YF-115?oldid=698158348.
- YF-115 isPrimaryTopicOf YF-115.