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- YF-75 abstract "The YF-75 is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a gas generator cycle. It is China's second generation of cryogenic propellant engine, after the YF-73, which it replaced. It is used in a dual engine mount in the H-18 third stage of the Long March 3A, Long March 3B and Long March 3C launch vehicles. Within the mount, each engine can gimbal individually to enable thrust vectoring control. The engine also heats hydrogen and helium to pressurize the stage tanks and can control the mixture ratio to optimize propellant consumption.".
- YF-75 wikiPageExternalLink yf75.htm.
- YF-75 wikiPageExternalLink engine.htm.
- YF-75 wikiPageExternalLink 200703181313154a301a.asp.
- YF-75 wikiPageID "12888952".
- YF-75 wikiPageLength "6521".
- YF-75 wikiPageOutDegree "40".
- YF-75 wikiPageRevisionID "695165473".
- YF-75 wikiPageWikiLink Beijing_Aerospace_Propulsion_Institute.
- YF-75 wikiPageWikiLink Category:Rocket_engines.
- YF-75 wikiPageWikiLink Category:Rocket_engines_of_China.
- YF-75 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- YF-75 wikiPageWikiLink Category:Spaceflight.
- YF-75 wikiPageWikiLink China.
- YF-75 wikiPageWikiLink China_Academy_of_Launch_Vehicle_Technology.
- YF-75 wikiPageWikiLink Cryogenic_fuel.
- YF-75 wikiPageWikiLink Cryogenic_rocket_engine.
- YF-75 wikiPageWikiLink Gas-generator_cycle.
- YF-75 wikiPageWikiLink Gimbaled_thrust.
- YF-75 wikiPageWikiLink Hydraulic_fluid.
- YF-75 wikiPageWikiLink Liquid-propellant_rocket.
- YF-75 wikiPageWikiLink Liquid_hydrogen.
- YF-75 wikiPageWikiLink Liquid_oxygen.
- YF-75 wikiPageWikiLink Long_March_3A.
- YF-75 wikiPageWikiLink Long_March_3B.
- YF-75 wikiPageWikiLink Long_March_3C.
- YF-75 wikiPageWikiLink Long_March_5.
- YF-75 wikiPageWikiLink Pyrotechnic_initiator.
- YF-75 wikiPageWikiLink RL10.
- YF-75 wikiPageWikiLink Regenerative_cooling_(rocket).
- YF-75 wikiPageWikiLink Revolutions_per_minute.
- YF-75 wikiPageWikiLink Rocket_engine.
- YF-75 wikiPageWikiLink Rocket_propellant.
- YF-75 wikiPageWikiLink Thrust_vectoring.
- YF-75 wikiPageWikiLink YF-73.
- YF-75 wikiPageWikiLink YF-75D.
- YF-75 wikiPageWikiLinkText "YF-75".
- YF-75 associated "--03-03".
- YF-75 combustionChamber "1".
- YF-75 countryOfOrigin China.
- YF-75 cycle Gas-generator_cycle.
- YF-75 designer Beijing_Aerospace_Propulsion_Institute.
- YF-75 firstDate "1994-02-08".
- YF-75 fuel Liquid_hydrogen.
- YF-75 manufacturer China_Academy_of_Launch_Vehicle_Technology.
- YF-75 mixtureRatio "5.1".
- YF-75 name "YF-75".
- YF-75 nozzleRatio "80".
- YF-75 oxidizer Liquid_oxygen.
- YF-75 predecessor YF-73.
- YF-75 status "In service".
- YF-75 successor YF-75D.
- YF-75 type "liquid".
- YF-75 usedIn "--03-03".
- YF-75 wikiPageUsesTemplate Template:Convert.
- YF-75 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- YF-75 wikiPageUsesTemplate Template:Reflist.
- YF-75 wikiPageUsesTemplate Template:Rocket_Engines.
- YF-75 subject Category:Rocket_engines.
- YF-75 subject Category:Rocket_engines_of_China.
- YF-75 subject Category:Rocket_engines_using_hydrogen_propellant.
- YF-75 subject Category:Spaceflight.
- YF-75 hypernym Hydrogen.
- YF-75 type MeanOfTransportation.
- YF-75 type Technology.
- YF-75 comment "The YF-75 is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a gas generator cycle. It is China's second generation of cryogenic propellant engine, after the YF-73, which it replaced. It is used in a dual engine mount in the H-18 third stage of the Long March 3A, Long March 3B and Long March 3C launch vehicles. Within the mount, each engine can gimbal individually to enable thrust vectoring control.".
- YF-75 label "YF-75".
- YF-75 sameAs Q8045876.
- YF-75 sameAs YF-75.
- YF-75 sameAs YF-75.
- YF-75 sameAs YF-75.
- YF-75 sameAs m.02x9z7f.
- YF-75 sameAs Q8045876.
- YF-75 sameAs YF-75.
- YF-75 wasDerivedFrom YF-75?oldid=695165473.
- YF-75 homepage engine.htm.
- YF-75 isPrimaryTopicOf YF-75.