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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:aircraft_operated
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gptkb:F/_A-18_family
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gptkbp:application
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gptkb:battle
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|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
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|
gptkbp:cooling_system
|
air-cooled
air-cooled system
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|
gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:engine
|
gptkb:General_Electric_Aviation
gptkb:F414_series
fighter jets
high reliability
Brayton cycle
high efficiency
F404-GE-400
twin-spool
twin-shaft
16,500 lbf without afterburner
|
|
gptkbp:engine_type
|
gptkb:F414
turbofan
axial compressor
high-pressure turbine
|
|
gptkbp:first_flight
|
gptkb:1995
|
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gptkbp:fuel_capacity
|
4.8 m
1,588 kg
0.8 lb/hp/hr
1.02 m
|
|
gptkbp:fuel_type
|
gptkb:JP-5
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 S
|
|
gptkbp:length
|
15 ft 8 in
|
|
gptkbp:maintenance
|
low maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:notable_features
|
reduced maintenance costs
|
|
gptkbp:operational_area
|
gptkb:aircraft
|
|
gptkbp:propulsion
|
gptkb:battle
22,000 lbf
|
|
gptkbp:services
|
gptkb:1999
|
|
gptkbp:successor
|
gptkb:F414-GE-400
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:weight
|
3,500 lb
|
|
gptkbp:bfsParent
|
gptkb:F414_Engine
gptkb:Pratt_&_Whitney_F414
|
|
gptkbp:bfsLayer
|
5
|