|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
F-35 family
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:compressionRatio
|
30:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital
|
|
gptkbp:coolingSystem
|
air
air-cooled
|
|
gptkbp:designedFor
|
F-35 Lightning II
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:emissionsStandard
|
low
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
4.9 m
modular design
air start
pylon-mounted
1,360 kg
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineDisplacement
|
1.1 m
|
|
gptkbp:engineType
|
high-pressure turbine
military turbofan
FAA_certified
|
|
gptkbp:fanBase
|
wide-chord fan
|
|
gptkbp:firstFlight
|
2006
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
gptkbp:hasArea
|
extensive ground testing
|
|
gptkbp:hasContent
|
0.5 lb/hp/hr
|
|
gptkbp:hasDepartment
|
yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-600
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:maxSpeed
|
gptkb:Mach_1.6
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:numberBuilt
|
over 1,000
|
|
gptkbp:operationalStatus
|
in service
up to 1,600 °C
|
|
gptkbp:partOf
|
Joint Strike Fighter program
|
|
gptkbp:productionCompany
|
$10 million per unit
|
|
gptkbp:propulsion
|
yes
43,000 lbf
28:1
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:replacedBy
|
F119-PW-100
|
|
gptkbp:services
|
50,000 ft
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
future upgrades planned
|
|
gptkbp:variant
|
F119-PW-100
|
|
gptkbp:weight
|
3,000 lb
|