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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:budget
|
$10 million per unit
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
36 in
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
F404-GE-400
air start
|
|
gptkbp:engine_configuration
|
twin-spool
twin-spool axial flow
|
|
gptkbp:engine_power
|
6,000 hours
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_capacity
|
4.1 m
0.91 m
1,270 kg
|
|
gptkbp:fuel_economy
|
high
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 T
|
|
gptkbp:length
|
160 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 1.8
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:operational_range
|
1,250 nautical miles
|
|
gptkbp:propulsion
|
no
7.7
22,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F/_A-18_Super_Hornet
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1999
|
|
gptkbp:successor
|
gptkb:F414-GE-400
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
|
gptkbp:bfsLayer
|
8
|