gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:Boeing_X-32
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gptkbp:application
|
air superiority fighter
|
gptkbp:certification
|
military certification achieved
|
gptkbp:check_in_time
|
yes
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gptkbp:combustor_type
|
annular
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gptkbp:compressor_type
|
gptkb:3
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gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
|
advanced cooling techniques
|
gptkbp:design
|
low observable
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gptkbp:development
|
gptkb:F119_engine_family
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gptkbp:diameter
|
1.2 m
1.1 m
|
gptkbp:engine
|
gptkb:F119_family
gptkb:stealth_technology
advanced materials
Brayton cycle
ongoing upgrades planned
F120
mass production initiated
|
gptkbp:engine_configuration
|
modular design
twin-engine
detailed specifications available
twin-engine layout
|
gptkbp:engine_development_program
|
gptkb:Joint_Strike_Fighter_program
|
gptkbp:engine_power
|
high reliability
high fuel efficiency
supercruise capability
|
gptkbp:engine_thrust_output
|
variable thrust output
|
gptkbp:engine_thrust_vectoring_capability
|
yes
|
gptkbp:engine_type
|
gptkb:F119-PW-100
high bypass turbofan
|
gptkbp:fuel_capacity
|
1.2 m
3.8 m
680 kg
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
https://www.w3.org/2000/01/rdf-schema#label
|
twin Pratt & Whitney F119-PW-100
|
gptkbp:is_tested_for
|
extensive testing conducted
|
gptkbp:length
|
3.8 m
|
gptkbp:maintenance
|
low maintenance requirements
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
gptkbp:noise_level
|
yes
|
gptkbp:notable_feature
|
stealth capabilities
|
gptkbp:operational_range
|
long operational range
|
gptkbp:operational_use
|
gptkb:military
|
gptkbp:original_run
|
gptkb:1996
|
gptkbp:propulsion
|
0.23
yes
28,000 lbf
35,000 lbf with afterburner
28,000 lbf without afterburner
|
gptkbp:service_entry
|
gptkb:2005
|
gptkbp:turbine_type
|
2
|
gptkbp:type
|
gptkb:turbofan_engine
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
gptkbp:weight
|
1,500 lb
|
gptkbp:bfsParent
|
gptkb:Lockheed_YF-22
|
gptkbp:bfsLayer
|
7
|