|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
multirole stealth fighter
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:competes_with
|
gptkb:Rolls-Royce_F136
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
used for cabin pressurization
|
|
gptkbp:customer_support
|
gptkb:United_States_Air_Force
|
|
gptkbp:development
|
gptkb:Joint_Strike_Fighter_program
|
|
gptkbp:development_cost
|
$1.5 billion
|
|
gptkbp:diameter
|
81 inches
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:features
|
stealth capabilities
|
|
gptkbp:first_flight
|
gptkb:2006
|
|
gptkbp:fuel_capacity
|
3.5 ft
16.5 ft
|
|
gptkbp:fuel_economy
|
high
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney F135
|
|
gptkbp:introduced
|
gptkb:2006
|
|
gptkbp:is_tested_for
|
done at NASA Glenn Research Center
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
1,380 miles
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:part_of
|
gptkb:F-35_program
|
|
gptkbp:power_output
|
29,000 lbf without afterburner
43,000 lbf with afterburner
|
|
gptkbp:powers
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:propulsion
|
up to 43,000 lbf
|
|
gptkbp:reach
|
used by multiple countries
|
|
gptkbp:related_aircraft
|
gptkb:F-35_A
gptkb:F-35_B
gptkb:F-35_C
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:sustainment_cost
|
$1 trillion over 50 years
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:type_of
|
gptkb:turbofan_engine
|
|
gptkbp:upgrades
|
planned for enhanced performance
|
|
gptkbp:used_in
|
gptkb:F-35_Lightning_II
|
|
gptkbp:variant
|
gptkb:F135-PW-100
gptkb:F135-PW-600_(STOVL)
gptkb:F135-PW-600
gptkb:F135-PW-100_(CTOL)
F135-PW-100 (CV)
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:F-35_Lightning_II
gptkb:F-35_B_Lightning_II
|
|
gptkbp:bfsLayer
|
4
|