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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
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gptkb:F-22_Raptor
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|
gptkbp:cancellation_reason
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gptkb:battle
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
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gptkb:battle
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|
gptkbp:controls
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
advanced cooling technology
advanced cooling systems
|
|
gptkbp:design
|
modular design
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|
gptkbp:developer
|
gptkb:Joint_Strike_Fighter_program
|
|
gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:emissions_standard
|
low emissions
variable area intake
|
|
gptkbp:engine
|
gptkb:aircraft
gptkb:F119_family
high performance
advanced materials
high reliability
ongoing upgrades
Brayton cycle
ongoing development
advanced engine technology
state-of-the-art design
performance metrics available
detailed specifications
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|
gptkbp:engine_type
|
gptkb:F119-PW-100
axial compressor
high-pressure turbine
|
|
gptkbp:features
|
supercruise capability
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.5 lb/lbf/hr
16.5 ft
3.4 ft
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-700 Engine
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:operational_area
|
gptkb:2005
|
|
gptkbp:operational_range
|
1,839 miles
|
|
gptkbp:power_output
|
twin-engine configuration
|
|
gptkbp:propulsion
|
gptkb:battle
35,000 lbf
27,000 lbf without afterburner
35,000 lbf with afterburner
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|