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- YF-75 abstract "The YF-75 is China's second generation of cryogenic gimballed engine, using liquid hydrogen (LH2) fuel and liquid oxygen (LOX) oxidizer. Its development began in the early 1990s and its first flight was in 1994.".
- YF-75 wikiPageExternalLink engine.htm.
- YF-75 wikiPageExternalLink yf75.htm.
- YF-75 wikiPageExternalLink 200703181313154a301a.asp.
- YF-75 wikiPageID "12888952".
- YF-75 wikiPageRevisionID "605141319".
- YF-75 combustionChamber "1".
- YF-75 countryOfOrigin "China".
- YF-75 cycle Gas-generator_cycle.
- YF-75 fuel Liquid_hydrogen.
- YF-75 hasPhotoCollection YF-75.
- YF-75 manufacturer China_Academy_of_Launch_Vehicle_Technology.
- YF-75 mixtureRatio "5".
- YF-75 name "YF-75".
- YF-75 nozzleRatio "80".
- YF-75 oxidizer Liquid_oxygen.
- YF-75 status "In service & development".
- YF-75 type "liquid".
- YF-75 usedIn "--03-03".
- YF-75 subject Category:Hydrogen_rocket_engines.
- YF-75 subject Category:Rocket_engines_of_China.
- YF-75 comment "The YF-75 is China's second generation of cryogenic gimballed engine, using liquid hydrogen (LH2) fuel and liquid oxygen (LOX) oxidizer. Its development began in the early 1990s and its first flight was in 1994.".
- YF-75 label "YF-75".
- YF-75 label "YF-75".
- YF-75 sameAs YF-75.
- YF-75 sameAs YF-75.
- YF-75 sameAs m.02x9z7f.
- YF-75 sameAs Q8045876.
- YF-75 sameAs Q8045876.
- YF-75 wasDerivedFrom YF-75?oldid=605141319.
- YF-75 isPrimaryTopicOf YF-75.