|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
gptkb:KAI_T-50_Golden_Eagle
gptkb:McDonnell_Douglas_F/A-18_Hornet
gptkb:Northrop_F-20_Tigershark
gptkb:Dassault_Rafale_(early_prototypes)
|
|
gptkbp:bypassRatio
|
0.34:1
|
|
gptkbp:compressionRatio
|
fan + 7-stage axial compressor
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
35 inches
|
|
gptkbp:firstFlight
|
1977
|
|
gptkbp:fuelType
|
gptkb:Jet-A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric F404
|
|
gptkbp:length
|
154 inches
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notableFeature
|
modular design
high reliability
fast throttle response
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:General_Electric_F414
|
|
gptkbp:thrust
|
48.9 kN
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedBy
|
gptkb:United_States_Navy
gptkb:Republic_of_Korea_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Finnish_Air_Force
gptkb:Spanish_Air_Force
gptkb:Royal_Malaysian_Air_Force
gptkb:Swiss_Air_Force
|
|
gptkbp:usedIn
|
gptkb:aircraft
|
|
gptkbp:weight
|
1,982 lb
|
|
gptkbp:bfsParent
|
gptkb:F-20_Tigershark
gptkb:X-29
gptkb:Tejas
|
|
gptkbp:bfsLayer
|
6
|