gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F110
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gptkbp:aircraft_operated
|
F-22 Raptor integration
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gptkbp:application
|
gptkb:aircraft
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gptkbp:average_temperature
|
1,600 ° F
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gptkbp:competitors
|
gptkb:GE_F120
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gptkbp:contract
|
gptkb:1989
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
gptkbp:design
|
stealth capability
|
gptkbp:developed_by
|
gptkb:Pratt_&_Whitney
|
gptkbp:developer
|
gptkb:1986
$2 billion
|
gptkbp:diameter
|
1.2 m
1.1 m
|
gptkbp:emissions_standard
|
low emissions
|
gptkbp:engine
|
twin-spool
air start
|
gptkbp:engine_type
|
gptkb:3
2
|
gptkbp:environmental_impact
|
reduced environmental impact
|
gptkbp:features
|
vectoring thrust
|
gptkbp:first_flight
|
gptkb:1997
|
gptkbp:fuel_capacity
|
high efficiency
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
gptkbp:global_presence
|
used by US Air Force
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119 engine program
|
gptkbp:invention
|
multiple patents filed
Y F119
|
gptkbp:is_tested_for
|
gptkb:NASA_Langley_Research_Center
|
gptkbp:length
|
3.8 m
|
gptkbp:maintenance
|
4,000 hours
|
gptkbp:noise_level
|
low noise
|
gptkbp:notable_feature
|
supercruise capability
|
gptkbp:part_of
|
gptkb:Joint_Strike_Fighter_program
|
gptkbp:partnerships
|
collaboration with military branches
|
gptkbp:propulsion
|
5:1
70,000 lbf
35,000 lbf
|
gptkbp:publishes
|
numerous technical papers published
|
gptkbp:replaced_by
|
F120 engine
|
gptkbp:research_and_development
|
ongoing R& D efforts
|
gptkbp:safety_record
|
excellent safety record
|
gptkbp:services
|
gptkb:2005
|
gptkbp:supports
|
1,200 lb/s
|
gptkbp:sustainability
|
sustainable aviation fuel compatible
|
gptkbp:training
|
pilot training programs
|
gptkbp:type
|
gptkb:engine
|
gptkbp:upgrades
|
planned upgrades for performance
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
gptkbp:weight
|
1,500 lb
|