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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:Boeing_P-8_Poseidon
gptkb:Mc_Donnell_Douglas_C-17_Globemaster_III
|
|
gptkbp:aircraft_operated
|
gptkb:F-22_family
|
|
gptkbp:application
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gptkb:aircraft
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
gptkb:battle
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|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling system
|
|
gptkbp:design
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:developer
|
ongoing
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
gptkb:F119_series
gptkb:F119-PW-100
gptkb:advanced_technology
gptkb:F119_family
high performance
modular design
air superiority missions
mass production
high reliability
stealth capabilities
high efficiency
twin-spool
frequent upgrades
extensive operational history
F117-PW-100
cutting-edge innovations
long lifecycle
various performance metrics
detailed specifications
rich development history
military thrust rating
numerous advancements
various military aircrafts
|
|
gptkbp:engine_type
|
gptkb:F117
gptkb:F117-PW-101
axial compressor
high bypass turbofan
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney F117-PW-100
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_range
|
1,839 km
|
|
gptkbp:propulsion
|
gptkb:battle
24:1
29,000 lbf
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,200 kg
|