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- YF-50t abstract "The YF-50t is a Chinese cryogenic rocket engine being developed to power the upper stages of the Long March 5 family of launch vehicles. It is an indigenous development based on Chinese experience with the YF-73 and YF-75 upper stage engines. It is gimballed in two axes. Hydrogen bled from the engine is used to pressurize the oxygen tank, and helium is used to pressurize the hydrogen tank.".
- YF-50t wikiPageExternalLink yf50t.htm.
- YF-50t wikiPageID "24110042".
- YF-50t wikiPageLength "1440".
- YF-50t wikiPageOutDegree "14".
- YF-50t wikiPageRevisionID "699955730".
- YF-50t wikiPageWikiLink Category:Rocket_engines_of_China.
- YF-50t wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- YF-50t wikiPageWikiLink China.
- YF-50t wikiPageWikiLink Liquid_hydrogen.
- YF-50t wikiPageWikiLink Liquid_oxygen.
- YF-50t wikiPageWikiLink Long_March_5.
- YF-50t wikiPageWikiLink Rocket_engine.
- YF-50t wikiPageWikiLink Staged_combustion_cycle.
- YF-50t wikiPageWikiLink YF-73.
- YF-50t wikiPageWikiLink YF-75.
- YF-50t wikiPageWikiLink YF-75D.
- YF-50t wikiPageWikiLink YF-77.
- YF-50t wikiPageWikiLinkText "YF-50t".
- YF-50t combustionChamber "1".
- YF-50t countryOfOrigin China.
- YF-50t cycle Staged_combustion_cycle.
- YF-50t date "2003".
- YF-50t designer "CAALPT".
- YF-50t fuel Liquid_hydrogen.
- YF-50t name "YF-50t".
- YF-50t oxidiser Liquid_oxygen.
- YF-50t purpose "Upper stage booster".
- YF-50t status "Under Development".
- YF-50t thrust(sl)_ "540 kN".
- YF-50t thrust(vac)_ "700 kN".
- YF-50t type "liquid".
- YF-50t wikiPageUsesTemplate Template:Convert.
- YF-50t wikiPageUsesTemplate Template:Infobox_rocket_engine.
- YF-50t wikiPageUsesTemplate Template:Reflist.
- YF-50t wikiPageUsesTemplate Template:Rocket_Engines.
- YF-50t subject Category:Rocket_engines_of_China.
- YF-50t subject Category:Rocket_engines_using_hydrogen_propellant.
- YF-50t hypernym Engine.
- YF-50t type Software.
- YF-50t type Technology.
- YF-50t comment "The YF-50t is a Chinese cryogenic rocket engine being developed to power the upper stages of the Long March 5 family of launch vehicles. It is an indigenous development based on Chinese experience with the YF-73 and YF-75 upper stage engines. It is gimballed in two axes. Hydrogen bled from the engine is used to pressurize the oxygen tank, and helium is used to pressurize the hydrogen tank.".
- YF-50t label "YF-50t".
- YF-50t sameAs Q16821933.
- YF-50t sameAs YF-50t.
- YF-50t sameAs m.07kg8rc.
- YF-50t sameAs Q16821933.
- YF-50t wasDerivedFrom YF-50t?oldid=699955730.
- YF-50t isPrimaryTopicOf YF-50t.