|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:stealth_technology
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development
|
gptkb:United_States_Air_Force
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
reduced
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:exported_to
|
allied nations
|
|
gptkbp:facilities
|
Pratt & Whitney test facility
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
gptkbp:has_documentation
|
provided to users
|
|
gptkbp:has_programs
|
gptkb:Joint_Advanced_Strike_Technology_(JAST)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-101
|
|
gptkbp:invention
|
numerous
|
|
gptkbp:involved_technology
|
gptkb:stealth_technology
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
long
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_use
|
gptkb:2005
|
|
gptkbp:performance
|
supercruise
|
|
gptkbp:project
|
planned improvements
|
|
gptkbp:propulsion
|
12.5:1
35,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-35_Lightning_II
gptkb:F-22_family
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:services_provided
|
available globally
|
|
gptkbp:sustainability
|
advanced materials
|
|
gptkbp:training_programs
|
offered to operators
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:upgrades
|
available
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F119
|
|
gptkbp:bfsLayer
|
5
|