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- YF-20 abstract "The YF-20 is a Chinese liquid rocket engine burning N2O4 and UDMH in an gas generator cycle. It is a basic engine which when mounted in a four engine module forms the YF-21. The high altitude variation is known as the YF-22 is normally paired with the YF-23 vernier to form the YF-24 propulsion module for second stages. New versions when used individually for booster applications are called YF-25.".
- YF-20 thumbnail YF-24B.JPG?width=300.
- YF-20 wikiPageID "47257502".
- YF-20 wikiPageLength "10017".
- YF-20 wikiPageOutDegree "41".
- YF-20 wikiPageRevisionID "695165426".
- YF-20 wikiPageWikiLink Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-20 wikiPageWikiLink Category:Rocket_engines.
- YF-20 wikiPageWikiLink Category:Rocket_engines_of_China.
- YF-20 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- YF-20 wikiPageWikiLink China.
- YF-20 wikiPageWikiLink Dinitrogen_tetroxide.
- YF-20 wikiPageWikiLink Feng_Bao_1.
- YF-20 wikiPageWikiLink Gas-generator_cycle.
- YF-20 wikiPageWikiLink Government_of_China.
- YF-20 wikiPageWikiLink Liquid-propellant_rocket.
- YF-20 wikiPageWikiLink Long_March_(rocket_family).
- YF-20 wikiPageWikiLink Long_March_2A.
- YF-20 wikiPageWikiLink Long_March_2C.
- YF-20 wikiPageWikiLink Long_March_2D.
- YF-20 wikiPageWikiLink Long_March_2E.
- YF-20 wikiPageWikiLink Long_March_2_(rocket_family).
- YF-20 wikiPageWikiLink Long_March_3.
- YF-20 wikiPageWikiLink Long_March_3A.
- YF-20 wikiPageWikiLink Long_March_3B.
- YF-20 wikiPageWikiLink Long_March_4A.
- YF-20 wikiPageWikiLink Northrop_YF-23.
- YF-20 wikiPageWikiLink Rocket_engine.
- YF-20 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- YF-20 wikiPageWikiLink Vernier_thruster.
- YF-20 wikiPageWikiLink YF-23_(rocket_engine).
- YF-20 wikiPageWikiLinkText "YF-20".
- YF-20 wikiPageWikiLinkText "YF-20A".
- YF-20 wikiPageWikiLinkText "YF-20B".
- YF-20 wikiPageWikiLinkText "YF-21B".
- YF-20 wikiPageWikiLinkText "YF-21C".
- YF-20 wikiPageWikiLinkText "YF-24B".
- YF-20 wikiPageWikiLinkText "YF-24C".
- YF-20 wikiPageWikiLinkText "YF-24D".
- YF-20 wikiPageWikiLinkText "YF-24E".
- YF-20 wikiPageWikiLinkText "YF-25".
- YF-20 associated "--03-02".
- YF-20 burnTime "160.0".
- YF-20 caption "A YF-24B engine".
- YF-20 combustionChamber "1".
- YF-20 countryOfOrigin China.
- YF-20 cycle Gas-generator_cycle.
- YF-20 designer Academy_of_Aerospace_Liquid_Propulsion_Technology.
- YF-20 firstDate "1995-06-01".
- YF-20 fuel Unsymmetrical_dimethylhydrazine.
- YF-20 gimbal "±10°".
- YF-20 name "YF-20B".
- YF-20 nozzleRatio "12.69".
- YF-20 oxidiser Dinitrogen_tetroxide.
- YF-20 status "In Production".
- YF-20 type "liquid".
- YF-20 usedIn "--03-02".
- YF-20 wikiPageUsesTemplate Template:Convert.
- YF-20 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- YF-20 wikiPageUsesTemplate Template:Reflist.
- YF-20 wikiPageUsesTemplate Template:Rocket_Engines.
- YF-20 subject Category:Rocket_engines.
- YF-20 subject Category:Rocket_engines_of_China.
- YF-20 subject Category:Rocket_engines_using_hypergolic_propellant.
- YF-20 hypernym O.
- YF-20 type Person.
- YF-20 comment "The YF-20 is a Chinese liquid rocket engine burning N2O4 and UDMH in an gas generator cycle. It is a basic engine which when mounted in a four engine module forms the YF-21. The high altitude variation is known as the YF-22 is normally paired with the YF-23 vernier to form the YF-24 propulsion module for second stages. New versions when used individually for booster applications are called YF-25.".
- YF-20 label "YF-20".
- YF-20 sameAs Q20944070.
- YF-20 sameAs YF-20.
- YF-20 sameAs Q20944070.
- YF-20 wasDerivedFrom YF-20?oldid=695165426.
- YF-20 depiction YF-24B.JPG.
- YF-20 isPrimaryTopicOf YF-20.