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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combat_radius
|
1,250 km
|
|
gptkbp:combat_role
|
air superiority
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:commissioned
|
gptkb:1996
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:development
|
gptkb:1980s
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
reduced emissions
|
|
gptkbp:engine
|
gptkb:F414-GE-400
air start
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_power
|
high performance
|
|
gptkbp:engine_type
|
military turbofan
|
|
gptkbp:exported_to
|
multiple countries
|
|
gptkbp:first_flight
|
gptkb:1999
|
|
gptkbp:fuel_economy
|
low
high
|
|
gptkbp:fuel_type
|
gptkb:JP-5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 Y
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:military_technology
|
no
yes
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_features
|
digital engine control system
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:propulsion
|
no
22,000 lbf
14.67
|
|
gptkbp:related_aircraft
|
multirole fighter
|
|
gptkbp:replaces
|
gptkb:F404_engine
|
|
gptkbp:service
|
6,000 hours
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
F404-GE-402
|
|
gptkbp:sustainability
|
environmentally friendly
|
|
gptkbp:training
|
advanced training
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:variant
|
F414 engine family
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
|
gptkbp:bfsLayer
|
8
|