| dbo:description
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- Turboréacteur (fr)
- motore aeronautico turbogetto (it)
- 1946 USAF's first axial-flow compressor engine (en)
- US-amerikanisches Turbojet-Triebwerk (de)
- proudový motor (cs)
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| dbo:thumbnail
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| dbo:wikiPageExternalLink
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| dbp:aircon
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| dbp:combustion
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- eight tubular inter-connected combustion chambers (en)
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| dbp:compression
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| dbp:compressor
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| dbp:developedInto
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| dbp:diameter
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- *Frontal area: (en)
- 37.0 (dbd:inch)
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| dbp:firstRun
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| dbp:fueltype
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- aviation kerosene, JP-4, MIL-F-5624 or 100/130 octane gasoline (en)
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| dbp:jetpipetemp
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| dbp:length
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- including afterburner (en)
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| dbp:lists
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- * List of aircraft engines (en)
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| dbp:majorApplications
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| dbp:manufacturer
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| dbp:nationalOrigin
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| dbp:numberBuilt
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| dbp:oilsystem
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- dry sump pressure system with spur gear pressure and scavenge pumps at (en)
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| dbp:ref
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- , Aircraft engines of the World 1957 (en)
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| dbp:related
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- * Allison J71
* General Electric T31
* General Electric J47 (en)
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| dbp:similarEngines
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- * Rolls-Royce Avon
* Tumansky RD-9 (en)
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| dbp:specfuelcon
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| dbp:thrust
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- *Maximum thrust : for take-off at 8,000 rpm (en)
- : for take-off at 8,000 rpm (en)
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| dbp:thrust/weight
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| dbp:turbine
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- single-stage axial turbine (en)
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| dbp:type
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| dbp:weight
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- without afterburner; including afterburner (en)
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| dbp:wikiPageUsesTemplate
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| dct:subject
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| gold:hypernym
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| rdfs:label
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- Allison J35 (en)
- Allison J35 (cs)
- General Electric J35 (de)
- Allison J35 (fr)
- Allison J35 (it)
- アリソン J35 (ja)
- Allison J35 (pl)
- Allison J35-A-35 (pt)
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| owl:sameAs
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| prov:wasDerivedFrom
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| foaf:depiction
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| foaf:isPrimaryTopicOf
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| is dbo:wikiPageRedirects
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| is dbo:wikiPageWikiLink
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| is dbp:developedFrom
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