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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:armament
|
blisk design
|
|
gptkbp:average_temperature
|
high temperature
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:collaborations
|
gptkb:Lockheed_Martin
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country
|
multiple countries
|
|
gptkbp:design
|
8,000 hours
|
|
gptkbp:developer
|
$1.5 billion
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:drivetrain
|
integrated gearbox
|
|
gptkbp:elevation
|
up to 50,000 ft
|
|
gptkbp:emissions_standard
|
low emissions
variable area
|
|
gptkbp:engine
|
two-spool
|
|
gptkbp:facilities
|
Pratt & Whitney test facility
|
|
gptkbp:features
|
gptkb:aircraft
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
high efficiency
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-400 Engine
|
|
gptkbp:launch_date
|
30 seconds
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:part_of
|
gptkb:F-35_program
|
|
gptkbp:performance
|
meets military specifications
|
|
gptkbp:produced_by
|
over 1,000
|
|
gptkbp:production_years
|
gptkb:2005
|
|
gptkbp:propulsion
|
gptkb:battle
43,000 lbf
9.5 lbf/lb
|
|
gptkbp:replaced_by
|
gptkb:F119-PW-100
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_record
|
excellent safety record
|
|
gptkbp:services
|
gptkb:2006
comprehensive support services
|
|
gptkbp:sustainability
|
sustainable aviation fuel compatible
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:upgrades
|
planned upgrades
|
|
gptkbp:used_in
|
gptkb:star
|
|
gptkbp:weight
|
3,000 lb
|