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- Allison_J35 abstract "The General Electric/Allison J35 was originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based centrifugal-flow J33, and was the United States Air Force's first axial-flow (straight-through airflow) compressor engine. The J35 was fairly simple, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (32.92 kN).Like the J33, the design of the J35 originated at General Electric, but major production was by the Allison Engine Company.".
- Allison_J35 wikiPageExternalLink 1948%20-%201229.html.
- Allison_J35 wikiPageExternalLink J35.htm.
- Allison_J35 wikiPageID "1266099".
- Allison_J35 wikiPageRevisionID "604806737".
- Allison_J35 aircon "/ sec at take-off power".
- Allison_J35 combustion "Eight tubular inter-connected combustion chambers".
- Allison_J35 compression "5".
- Allison_J35 compressor "11".
- Allison_J35 developedInto Allison_J71.
- Allison_J35 firstRun "1946".
- Allison_J35 fueltype "Aviation kerosene, JP-4, MIL-F-5624 or 100/130 octane gasoline".
- Allison_J35 hasPhotoCollection Allison_J35.
- Allison_J35 jetpipetemp "maximum".
- Allison_J35 length "including afterburner".
- Allison_J35 lists "* List of aircraft engines".
- Allison_J35 majorApplications Northrop_F-89_Scorpion.
- Allison_J35 majorApplications Republic_F-84_Thunderjet.
- Allison_J35 manufacturer Allison_Engine_Company.
- Allison_J35 manufacturer GE_Aviation.
- Allison_J35 nationalOrigin United_States.
- Allison_J35 oilsystem "Dry sump pressure system with spur gear pressure and scavenge pumps at".
- Allison_J35 related "* General Electric J47 * Allison J71".
- Allison_J35 similarEngines "*Rolls-Royce Avon".
- Allison_J35 specfuelcon "1.1".
- Allison_J35 thrust "* at 8,000 rpm * with afterburner".
- Allison_J35 weight "2.53".
- Allison_J35 turbine "Single-stage axial".
- Allison_J35 type Turbojet.
- Allison_J35 type "Afterburning turbojet".
- Allison_J35 weight "dry, including afterburner".
- Allison_J35 subject Category:Allison_aircraft_engines.
- Allison_J35 subject Category:Turbojet_engines_1940–1949.
- Allison_J35 comment "The General Electric/Allison J35 was originally developed by General Electric (GE company designation TG-180) in parallel with the Whittle-based centrifugal-flow J33, and was the United States Air Force's first axial-flow (straight-through airflow) compressor engine. The J35 was fairly simple, consisting of an eleven-stage axial-flow compressor and a single-stage turbine.".
- Allison_J35 label "Allison J35".
- Allison_J35 label "Allison J35".
- Allison_J35 label "Allison J35".
- Allison_J35 label "General Electric J35".
- Allison_J35 sameAs General_Electric_J35.
- Allison_J35 sameAs Allison_J35.
- Allison_J35 sameAs Allison_J35.
- Allison_J35 sameAs m.04nhf_.
- Allison_J35 sameAs Q478153.
- Allison_J35 sameAs Q478153.
- Allison_J35 wasDerivedFrom Allison_J35?oldid=604806737.
- Allison_J35 isPrimaryTopicOf Allison_J35.