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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:average_temperature
|
high temperature
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gptkbp:certification
|
military certification
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gptkbp:combustor_type
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annular combustor
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gptkbp:compressor_type
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axial compressor
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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air-cooled
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gptkbp:customer_base
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gptkb:United_States_Navy
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gptkbp:design_features
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modular design
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gptkbp:development
|
ongoing development
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gptkbp:diameter
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36 in
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gptkbp:emissions_standard
|
low emissions
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gptkbp:engine_configuration
|
twin-spool
|
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gptkbp:fan_art
|
single-stage fan
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gptkbp:first_flight
|
gptkb:1999
|
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gptkbp:fuel_economy
|
high efficiency
0.8 lb/lbf/hr
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gptkbp:fuel_type
|
gptkb:JP-5
dual fuel system
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gptkbp:future_plans
|
future upgrades planned
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gptkbp:global_presence
|
used globally
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gptkbp:history
|
developed from F404 engine
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|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 J
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gptkbp:investment
|
30 psi
|
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gptkbp:is_tested_for
|
extensively tested
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gptkbp:length
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160 in
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gptkbp:maintenance
|
1,000 hours
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gptkbp:manufacturer
|
gptkb:General_Electric
|
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gptkbp:noise_level
|
low noise
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gptkbp:operational_use
|
combat operations
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gptkbp:performance
|
high performance
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gptkbp:propulsion
|
no
22,000 lbf
|
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gptkbp:related_aircraft
|
compatible with multiple aircraft
|
|
gptkbp:reliability
|
high reliability
|
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gptkbp:service
|
6,000 hours
|
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gptkbp:successor
|
F404-GE-400
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gptkbp:support
|
logistical support available
|
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gptkbp:turbine_type
|
high-pressure turbine
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gptkbp:type
|
afterburning turbofan
|
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gptkbp:upgrades
|
upgradeable to F414-GE-400 E
|
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gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
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gptkbp:weight
|
3,500 lb
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gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
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gptkbp:bfsLayer
|
8
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