F414-GE-400 F

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature high temperature
gptkbp:cancellation_reason yes
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
gptkbp:cooling_system air-cooled
gptkbp:design 6,000 hours
gptkbp:development_cost $1 billion
gptkbp:diameter 36 in
gptkbp:emissions_standard low emissions
gptkbp:engine modular design
F404-GE-400
air start
GE F414 family
gptkbp:engine_configuration twin-spool
gptkbp:exported_to gptkb:Australia
gptkbp:fighting_style yes
gptkbp:first_flight gptkb:1995
gptkbp:fuel_capacity 1,600 kg
gptkbp:fuel_economy high
high thrust-to-fuel ratio
gptkbp:fuel_type gptkb:JP-5
gptkbp:has_programs Navy's Enhanced Engine Program
https://www.w3.org/2000/01/rdf-schema#label F414-GE-400 F
gptkbp:is_tested_for extensive ground testing
gptkbp:length 160 in
gptkbp:maintenance 1,000 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:max_speed Mach 1.8
gptkbp:operational_range long range
gptkbp:operational_use gptkb:military_aircraft
gptkbp:partnerships collaboration with military
gptkbp:primary_user gptkb:United_States_Navy
gptkbp:project next generation engines
gptkbp:propulsion no
22,000 lbf
6.3:1
gptkbp:related_aircraft gptkb:F/_A-18_E/_F_Super_Hornet
gptkbp:reliability high
gptkbp:service_ceiling 50,000 ft
gptkbp:services_provided logistics support
gptkbp:successor F404-GE-400
gptkbp:sustainability environmentally friendly design
gptkbp:training_programs pilot training
gptkbp:turbine_type high bypass ratio
gptkbp:type afterburning turbofan
gptkbp:upgrades performance enhancements
gptkbp:used_in gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
gptkbp:variant gptkb:F414-GE-400_E
gptkbp:weight 3,500 lb
gptkbp:bfsParent gptkb:General_Electric_F414_engine
gptkbp:bfsLayer 8