gptkbp:instance_of
|
gptkb:jet_engine
|
gptkbp:application
|
multirole stealth fighter
|
gptkbp:average_temperature
|
high
|
gptkbp:check_in_time
|
yes
|
gptkbp:combustor_type
|
annular
|
gptkbp:compression_ratio
|
30:1
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
gptkbp:cooling_system
|
air-cooled
|
gptkbp:designed_for
|
gptkb:F-35_Lightning_II
|
gptkbp:development
|
gptkb:1996
gptkb:2006
|
gptkbp:development_cost
|
$1.5 billion
|
gptkbp:diameter
|
1.2 m
|
gptkbp:emissions_standard
|
low
|
gptkbp:engine_configuration
|
pylon-mounted
|
gptkbp:engine_type
|
single spool
|
gptkbp:exhaust_system
|
variable geometry
|
gptkbp:fan_art
|
wide-chord fan
|
gptkbp:first_flight
|
gptkb:2006
|
gptkbp:fuel_economy
|
high
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
https://www.w3.org/2000/01/rdf-schema#label
|
F135-PW-100 (CTOL)
|
gptkbp:integration
|
seamless with aircraft systems
|
gptkbp:launch_date
|
30 seconds
|
gptkbp:length
|
3.5 m
|
gptkbp:maintenance
|
1,000 hours
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
gptkbp:military_service
|
gptkb:United_States_Air_Force
|
gptkbp:noise_level
|
low
|
gptkbp:operational_range
|
1,380 km
|
gptkbp:operational_status
|
active
|
gptkbp:performance
|
superior
|
gptkbp:produces
|
high
|
gptkbp:production_years
|
gptkb:2007
|
gptkbp:propulsion
|
no
43,000 lbf
|
gptkbp:related_to
|
gptkb:F135-PW-400
gptkb:F135-PW-600
|
gptkbp:reliability
|
high
|
gptkbp:service_ceiling
|
15,240 m
|
gptkbp:shutdown_time
|
10 seconds
|
gptkbp:sustainability
|
high
|
gptkbp:technology
|
advanced materials
|
gptkbp:turbine_type
|
high-pressure turbine
single crystal superalloy
|
gptkbp:type
|
gptkb:turbofan_engine
|
gptkbp:used_in
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
gptkbp:user_countries
|
gptkb:Australia
gptkb:Italy
gptkb:Norway
gptkb:United_Kingdom
gptkb:United_States
|
gptkbp:variant
|
gptkb:F135_engine_family
|
gptkbp:weight
|
1,500 kg
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_F135
|
gptkbp:bfsLayer
|
5
|