|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
1,500 ° C
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
4,000 hours
|
|
gptkbp:development
|
F404-GE-400
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:exhaust_system
|
variable geometry
|
|
gptkbp:fan_art
|
single-stage fan
|
|
gptkbp:first_flight
|
gptkb:1983
|
|
gptkbp:first_introduced
|
gptkb:1983
|
|
gptkbp:fuel_economy
|
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:electronic
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F404 Engine
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:notable_users
|
gptkb:Kuwait_Air_Force
gptkb:Singapore_Air_Force
gptkb:Indian_Navy
gptkb:Royal_Air_Force
gptkb:United_States_Navy
gptkb:United_States_Marine_Corps
gptkb:Canadian_Forces
gptkb:Malaysia_Air_Force
gptkb:Thailand_Air_Force
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_range
|
1,200 nautical miles
|
|
gptkbp:power_output
|
16,000 to 22,000 lbf
|
|
gptkbp:propulsion
|
no
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:thrust_augmentation
|
afterburner
|
|
gptkbp:turbine_type
|
axial
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Grumman_F-14_Tomcat
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:variant
|
F404-GE-400
F404-GE-402
F404-GE-402 D
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:bfsLayer
|
5
|