|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:aircraft_operated
|
gptkb:star
F-22 and F-35
F-35 Lightning II (limited)
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,600 ° C
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling techniques
film cooling
|
|
gptkbp:design
|
modular
|
|
gptkbp:developer
|
gptkb:aircraft
1990s
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
low
variable geometry
Nox standard compliant
|
|
gptkbp:engine
|
gptkb:F119
gptkb:F119_family
over 1,000
twin-engine
Brayton cycle
superior
up to 8,000 hours
|
|
gptkbp:engine_type
|
axial
high bypass ratio
high-pressure turbine
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:exported_to
|
allied nations
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:feedback
|
positive
|
|
gptkbp:first_flight
|
gptkb:1997
gptkb:2005
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-100
|
|
gptkbp:integrates_with
|
seamless with aircraft systems
|
|
gptkbp:invention
|
multiple patents filed.
|
|
gptkbp:is_tested_for
|
completed
|
|
gptkbp:length
|
3.5 m
3.8 m
|
|
gptkbp:maintenance
|
1,500 hours
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:military_branch
|
gptkb:none
|
|
gptkbp:military_technology
|
air superiority missions
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_pieces
|
fewer than previous models
|
|
gptkbp:operational_area
|
gptkb:2005
active duty
|
|
gptkbp:operational_range
|
high altitude
1,839 km
|
|
gptkbp:original_run
|
gptkb:1996
|
|
gptkbp:part_of
|
gptkb:F-22_program
|
|
gptkbp:performance
|
superior
|
|
gptkbp:propulsion
|
gptkb:battle
high
22:1
35,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:sustainability
|
advanced materials
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
planned
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|