|
gptkbp:instanceOf
|
turbofan engine family
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:derivedFrom
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:developedBy
|
gptkb:Lockheed_Martin_F-35_Lightning_II
|
|
gptkbp:diameter
|
46 inches
|
|
gptkbp:firstFlight
|
2000
|
|
gptkbp:fuelType
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135 engine family
|
|
gptkbp:length
|
220 inches
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:notableFeature
|
modular design
advanced diagnostics
stealth compatibility
high thrust-to-weight ratio
integrated lift fan for STOVL (F-35B)
|
|
gptkbp:notableProgram
|
gptkb:Joint_Strike_Fighter_program
|
|
gptkbp:notableRelease
|
Enhanced Engine Package (EEP)
AETP (Adaptive Engine Transition Program) candidate
|
|
gptkbp:notableVariant
|
gptkb:F135-PW-100
gptkb:F135-PW-400
gptkb:F135-PW-600
|
|
gptkbp:primaryUser
|
gptkb:Royal_Netherlands_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Navy
gptkb:United_States_Air_Force
gptkb:United_States_Marine_Corps
gptkb:United_States_Navy
gptkb:Republic_of_Korea_Air_Force
gptkb:Royal_Danish_Air_Force
gptkb:Norwegian_Air_Force
gptkb:Israeli_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Finnish_Air_Force
gptkb:Italian_Air_Force
gptkb:Japan_Air_Self-Defense_Force
gptkb:Belgian_Air_Force
gptkb:Polish_Air_Force
gptkb:Singapore_Air_Force
|
|
gptkbp:relatedTo
|
gptkb:F119
gptkb:Rolls-Royce_LiftSystem
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:F119_engine
|
|
gptkbp:thrust
|
43,000 lbf
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedIn
|
gptkb:F-35A
gptkb:F-35B
gptkb:F-35C
|
|
gptkbp:weight
|
3,750 lb
|
|
gptkbp:bfsParent
|
gptkb:F135-PW-400
|
|
gptkbp:bfsLayer
|
8
|