F414-GE-400

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:average_temperature 1,600 ° C
gptkbp:certification military certification
gptkbp:combustor_type annular combustor
gptkbp:compressor_type axial compressor
gptkbp:control_system digital control system
gptkbp:cooling_system air-cooled
gptkbp:customer_support customer support services
gptkbp:design modular design
6,000 hours
gptkbp:diameter 1.1 m
gptkbp:emissions_standard low emissions
gptkbp:engine gptkb:F404_engine
Brayton cycle
gptkbp:facilities gptkb:test_subjects
gptkbp:first_flight gptkb:1995
gptkbp:fuel_economy high efficiency
gptkbp:fuel_type gptkb:JP-5
gptkbp:gearbox reduction gearbox
gptkbp:global_presence global presence
gptkbp:has_programs F414 development program
https://www.w3.org/2000/01/rdf-schema#label F414-GE-400
gptkbp:innovation engine innovation
gptkbp:investment high pressure
gptkbp:launch_date 30 seconds
gptkbp:length 3.8 m
gptkbp:maintenance 1,500 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:max_speed Mach 1.8
gptkbp:noise_level low noise
gptkbp:number_of_stages gptkb:10
gptkbp:partnerships industry partnerships
gptkbp:propulsion 22,000 lbf
14.67
gptkbp:replaced_by gptkb:F414-GE-400_EPE
gptkbp:research_and_development ongoing R& D
gptkbp:safety_record excellent safety record
gptkbp:service_entry gptkb:1999
gptkbp:supports ground support equipment
gptkbp:sustainability sustainable practices
gptkbp:training_programs training programs for operators
gptkbp:turbine_type high-pressure turbine
gptkbp:type afterburning turbofan engine
gptkbp:upgrades future upgrades planned
gptkbp:used_in gptkb:Boeing_F/_A-18_E/_F_Super_Hornet
gptkb:Mc_Donnell_Douglas_F/_A-18_Hornet
gptkbp:weight 1,500 kg
gptkbp:bfsParent gptkb:Super_Hornet
gptkb:F414_engine
gptkbp:bfsLayer 5