|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:X-35_Joint_Strike_Fighter
gptkb:F-117_Nighthawk
gptkb:Pratt_&_Whitney_F100
|
|
gptkbp:aircraft_operated
|
gptkb:F-22_Raptor
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:cancellation_reason
|
gptkb:battle
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling technology
|
|
gptkbp:design
|
low observable
|
|
gptkbp:developer
|
gptkb:aircraft
approximately $1 billion
|
|
gptkbp:diameter
|
approximately 3 ft
|
|
gptkbp:engine
|
gptkb:F119/_F135_family
modular design
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
gptkb:3
2
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:fuel_capacity
|
high
4.88 m
0.91 m
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
|
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_area
|
air superiority missions
|
|
gptkbp:operational_range
|
high subsonic to supersonic
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:propulsion
|
gptkb:battle
11:1
up to 35,000 lbf
|
|
gptkbp:service_ceiling
|
above 60,000 ft
|
|
gptkbp:successor
|
gptkb:Pratt_&_Whitney_F135
|
|
gptkbp:supports
|
approximately 30,000 lb/s
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
approximately 3,000 lb
|