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.

All labels observed (1)

Label Occurrences
General Electric J35 canonical 1

How this entity was disambiguated

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 ⓘ

How these facts were elicited

Referenced by (1)

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

General Electric J47 → developmentFrom → General Electric J35 ⓘ