|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:constructionMaterial
|
variable geometry
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:designedFor
|
F-35 Lightning II
|
|
gptkbp:developer
|
$1.5 billion
|
|
gptkbp:diameter
|
3.5 ft
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
4.9 m
air start
pylon-mounted
1,360 kg
|
|
gptkbp:engineConfiguration
|
twin-spool
digital control
|
|
gptkbp:engineDisplacement
|
1.1 m
|
|
gptkbp:engineType
|
gptkb:F135-PW-600_(CV)
gptkb:F135-PW-600
gptkb:F135-PW-600_(B)
gptkb:F135-PW-100_(CTOL)
2
3
high
air-cooled
afterburning turbofan
F135-PW-100
over 8,000 hours
F135-PW-100 (A)
F135-PW-100 (CV)
F135-PW-600 (STOVL)
|
|
gptkbp:firstFlight
|
2006
|
|
gptkbp:fuelType
|
Jet A
annular combustor
|
|
gptkbp:hasDepartment
|
yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney F135
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
long
|
|
gptkbp:manufacturer
|
gptkb:United_Technologies_Corporation
|
|
gptkbp:maxSpeed
|
gptkb:Mach_1.6
|
|
gptkbp:militaryRank
|
gptkb:United_States_Air_Force
gptkb:United_States_Navy
gptkb:United_States_Marine_Corps
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operatingHours
|
around 40:1
|
|
gptkbp:operationalStatus
|
high
in service
|
|
gptkbp:producedBy
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:propulsion
|
yes
43,000 lbf
28.5:1
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
2015
|
|
gptkbp:setting
|
single_spool
|
|
gptkbp:supports
|
ground support equipment
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
3,000 lb
|