|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
approximately 30,000 lb/s
|
|
gptkbp:application
|
gptkb:stealth_technology
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling technology
|
|
gptkbp:design
|
low observable
|
|
gptkbp:development
|
gptkb:United_States_Air_Force
|
|
gptkbp:development_cost
|
approximately $1 billion
|
|
gptkbp:diameter
|
approximately 3 ft
|
|
gptkbp:engine
|
gptkb:F119/_F135_family
modular design
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
gptkb:F119-PW-101
gptkb:F119-PW-102
gptkb:F119-PW-103
gptkb:F119-PW-104
gptkb:F119-PW-105
gptkb:F119-PW-106
gptkb:F119-PW-107
gptkb:F119-PW-108
gptkb:F119-PW-109
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:fuel_capacity
|
4.88 m
0.91 m
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney F119
|
|
gptkbp:length
|
approximately 16 ft
|
|
gptkbp:maintenance
|
longer intervals
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:operational_range
|
high subsonic to supersonic
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operational_use
|
air superiority missions
|
|
gptkbp:propulsion
|
yes
11:1
up to 35,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-22_Raptor
|
|
gptkbp:service_ceiling
|
above 60,000 ft
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_F135
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
approximately 3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:F-117_Nighthawk
|
|
gptkbp:bfsLayer
|
4
|