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gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
gptkb:KAI_KF-21_Boramae
gptkb:HAL_Tejas_Mk2
gptkb:Boeing_F/A-18E/F_Super_Hornet
Saab JAS 39E/F Gripen
|
|
gptkbp:bypassRatio
|
0.25:1
|
|
gptkbp:category
|
military aircraft engine
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:developedBy
|
GE F404
|
|
gptkbp:diameter
|
35 inches
|
|
gptkbp:family
|
General Electric F400 series
|
|
gptkbp:firstFlight
|
1996
|
|
gptkbp:fuelType
|
gptkb:Jet-A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE F414
|
|
gptkbp:length
|
154 inches
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:notableFeature
|
modular design
high thrust-to-weight ratio
|
|
gptkbp:numberOfStages
|
1 high-pressure, 1 low-pressure
3 fan, 7 high-pressure
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
GE F404
|
|
gptkbp:thrust
|
yes
22,000 lbf
|
|
gptkbp:usedIn
|
gptkb:F/A-18E/F_Super_Hornet
gptkb:KAI_KF-21_Boramae
gptkb:T-7A_Red_Hawk
gptkb:HAL_Tejas_Mk2
gptkb:EA-18G_Growler
Saab JAS 39E/F Gripen
|
|
gptkbp:weight
|
2,445 lb
|
|
gptkbp:bfsParent
|
gptkb:Advanced_Medium_Combat_Aircraft_(AMCA)
|
|
gptkbp:bfsLayer
|
7
|