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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
|
gptkb:star
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
wide-chord fan blades
|
|
gptkbp:average_temperature
|
high operating temperature
|
|
gptkbp:cancellation_reason
|
gptkb:battle
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:collaborations
|
collaboration with military
|
|
gptkbp:combat_role
|
air superiority
|
|
gptkbp:community_impact
|
global military impact
|
|
gptkbp:contribution
|
enhanced maneuverability
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:developer
|
1990s
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
Brayton cycle
twin-spool
annular combustor
|
|
gptkbp:engine_type
|
3 stages
2 stages
|
|
gptkbp:features
|
thrust vectoring
supercruise
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-400 Engine
|
|
gptkbp:innovation
|
engine innovation
|
|
gptkbp:integrates_with
|
integrated avionics
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:legacy
|
advanced stealth technology
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:operational_range
|
long operational range
|
|
gptkbp:part_of
|
gptkb:F-22_program
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:propulsion
|
gptkb:battle
high power-to-weight ratio
35,000 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:research_and_development
|
ongoing research and development
|
|
gptkbp:services
|
gptkb:2005
|
|
gptkbp:successor
|
gptkb:F135-PW-100
|
|
gptkbp:supports
|
logistics support
|
|
gptkbp:sustainability
|
focus on sustainability
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
future upgrades
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
1,800 lb
|