|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control system
|
|
gptkbp:cooling_system
|
air-cooled
intercooling system
|
|
gptkbp:diameter
|
36 in
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:military_aircraft
advanced materials
innovative technology
ongoing development
global support network
air start
|
|
gptkbp:engine_configuration
|
modular design
twin-spool
twin-spool turbofan
|
|
gptkbp:engine_power
|
high performance
6,000 hours
proven reliability
22,000 lbf thrust
|
|
gptkbp:engine_type
|
military engine
|
|
gptkbp:first_flight
|
gptkb:1999
|
|
gptkbp:fuel_capacity
|
3,500 lb
36 in
160 in
|
|
gptkbp:fuel_economy
|
high fuel efficiency
0.8 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F414-GE-400 D
|
|
gptkbp:investment
|
high pressure
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
160 in
|
|
gptkbp:maintenance
|
1,000 hours
low maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:propulsion
|
no
22,000 lbf
6.3:1
|
|
gptkbp:related_aircraft
|
gptkb:F/_A-18_E/_F_Super_Hornet
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_entry
|
gptkb:2001
|
|
gptkbp:successor
|
gptkb:F414-GE-400
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
afterburning turbofan engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
|
|
gptkbp:weight
|
3,500 lb
|
|
gptkbp:bfsParent
|
gptkb:General_Electric_F414_engine
|
|
gptkbp:bfsLayer
|
8
|