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- YF-100 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.".
- YF-100 wikiPageExternalLink 1532702682.html.
- YF-100 wikiPageID "12930143".
- YF-100 wikiPageLength "7967".
- YF-100 wikiPageOutDegree "37".
- YF-100 wikiPageRevisionID "681866718".
- YF-100 wikiPageWikiLink 863_Program.
- YF-100 wikiPageWikiLink Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-100 wikiPageWikiLink Category:Rocket_engines.
- YF-100 wikiPageWikiLink Category:Rocket_engines_of_China.
- YF-100 wikiPageWikiLink Category:Rocket_engines_using_kerosene_propellant.
- YF-100 wikiPageWikiLink Cavitation.
- YF-100 wikiPageWikiLink China.
- YF-100 wikiPageWikiLink First_stage_(rocketry).
- YF-100 wikiPageWikiLink Gimbaled_thrust.
- YF-100 wikiPageWikiLink Government_of_China.
- YF-100 wikiPageWikiLink Kerosene.
- YF-100 wikiPageWikiLink LOX.
- YF-100 wikiPageWikiLink Liquid-fuel_rocket.
- YF-100 wikiPageWikiLink Liquid-propellant_rocket.
- YF-100 wikiPageWikiLink Liquid_oxygen.
- YF-100 wikiPageWikiLink Long_March_5.
- YF-100 wikiPageWikiLink Long_March_6.
- YF-100 wikiPageWikiLink Long_March_7.
- YF-100 wikiPageWikiLink Multistage_rocket.
- YF-100 wikiPageWikiLink Pump-fed_engine.
- YF-100 wikiPageWikiLink RD-120.
- YF-100 wikiPageWikiLink RD-170.
- YF-100 wikiPageWikiLink RP-1.
- YF-100 wikiPageWikiLink Rocket.
- YF-100 wikiPageWikiLink Rocket_engine.
- YF-100 wikiPageWikiLink Rocket_propellant.
- YF-100 wikiPageWikiLink Staged_combustion_cycle.
- YF-100 wikiPageWikiLink Staged_combustion_cycle_(rocket).
- YF-100 wikiPageWikiLink YF-115.
- YF-100 wikiPageWikiLinkText "YF-100".
- YF-100 associated "--03-05".
- YF-100 burnTime "155.0".
- YF-100 combustionChamber "1".
- YF-100 countryOfOrigin China.
- YF-100 cycle "Oxidizer-rich Staged combustion".
- YF-100 designer Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-100 firstDate "2015-09-20".
- YF-100 fuel RP-1.
- YF-100 hasPhotoCollection YF-100.
- YF-100 mixtureRatio "2.6".
- YF-100 name "YF-100".
- YF-100 nozzleRatio "35".
- YF-100 oxidiser LOX.
- YF-100 oxidiser Liquid_oxygen.
- YF-100 predecessor RD-120.
- YF-100 status "In service".
- YF-100 throttleRange "65".
- YF-100 type "liquid".
- YF-100 usedIn "--03-05".
- YF-100 wikiPageUsesTemplate Template:Convert.
- YF-100 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- YF-100 wikiPageUsesTemplate Template:Reflist.
- YF-100 wikiPageUsesTemplate Template:Rocket-stub.
- YF-100 wikiPageUsesTemplate Template:Rocket_Engines.
- YF-100 wikiPageUsesTemplate Template:Since_when.
- YF-100 subject Category:Rocket_engines.
- YF-100 subject Category:Rocket_engines_of_China.
- YF-100 subject Category:Rocket_engines_using_kerosene_propellant.
- YF-100 hypernym LOX.
- YF-100 type Article.
- YF-100 type Article.
- YF-100 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.".
- YF-100 label "YF-100".
- YF-100 sameAs YF-100.
- YF-100 sameAs YF-100.
- YF-100 sameAs YF-100.
- YF-100 sameAs m.02z08kw.
- YF-100 sameAs Q11255036.
- YF-100 sameAs Q11255036.
- YF-100 wasDerivedFrom YF-100?oldid=681866718.
- YF-100 isPrimaryTopicOf YF-100.