General Electric J35

E925595

The General Electric J35 was an early American axial-flow turbojet engine that powered several first-generation U.S. jet aircraft in the late 1940s.

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Label Occurrences
General Electric J35 canonical 1

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Statements (31)

Predicate Object
instanceOf axial-flow turbojet engine
turbojet engine
application military aircraft propulsion
category aircraft engine
military jet engine
compressorType axial compressor
countryOfOrigin United States
developmentPeriod World War II and immediate postwar years
engineConfiguration single-spool
engineType axial-flow
era early jet age
fuelType kerosene-based jet fuel
historicalSignificance helped establish U.S. axial-flow jet engine technology
influenced Allison J33
later General Electric turbojet designs
manufacturer General Electric
notableFeature one of the first U.S.-designed axial-flow turbojets
powered Bell XP-83
Convair XP-81 (as a test installation)
Curtiss-Wright XP-87 Blackhawk
Northrop XP-89 (early development)
Republic F-84 Thunderjet (early variants, as Allison J35 license-build)
Republic XF-84H (test and development)
propulsionCycle Brayton cycle
role development engine for later U.S. jet engines
serviceEntryPeriod late 1940s
successor Allison J35
thrustClass early turbojet thrust range (on the order of several thousand pounds-force)
usedBy United States Air Force
usedFor flight testing of early jet aircraft prototypes
usedIn first-generation U.S. jet aircraft

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Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

General Electric J47 developmentFrom General Electric J35