|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
gptkb:fighter_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:General_Electric_Aviation
|
|
gptkbp:development
|
gptkb:F404_engine
|
|
gptkbp:diameter
|
36 in
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:General_Electric
F404-GE-400
air start
|
|
gptkbp:engine_configuration
|
twin-spool
twin-spool turbofan
|
|
gptkbp:engine_power
|
6,000 hours
16,000 k W
|
|
gptkbp:engine_test
|
ground test
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:F414-GE-400_U
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
1,600 kg
0.91 m
4.06 m
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 U
|
|
gptkbp:length
|
160 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:military_service
|
gptkb:United_States_Navy
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
long-range
|
|
gptkbp:propulsion
|
6.3
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1999
|
|
gptkbp:successor
|
F404-GE-400
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:variant
|
gptkb:F414-GE-400
|
|
gptkbp:weight
|
3,500 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
|
gptkbp:bfsLayer
|
8
|