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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:aircraft_type
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gptkb:stealth_technology
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:armament
|
blisk
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|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
8,000 hours
|
|
gptkbp:designed_for
|
gptkb:F-35_Lightning_II
|
|
gptkbp:development
|
gptkb:1999
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
Brayton cycle
air start
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:facilities
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:has_programs
|
gptkb:Joint_Strike_Fighter_Program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-400
|
|
gptkbp:investment
|
high
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:material
|
advanced alloys
|
|
gptkbp:max_speed
|
Mach 1.6
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_pieces
|
over 10,000
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:propulsion
|
yes
43,000 lbf
28:1
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:supply_chain
|
global supply chain
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:F135-PW-100_(CTOL)
|
|
gptkbp:bfsLayer
|
6
|