F135-PW-100 (CTOL)

GPTKB entity

Statements (59)
Predicate Object
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