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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:F-35_Lightning_II
|
|
gptkbp:application
|
gptkb:stealth_technology
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
30:1
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:development
|
1990s
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:advanced_technology
gptkb:F119_family
advanced materials
mass production
ongoing upgrades
Brayton cycle
multirole fighter
|
|
gptkbp:engine_configuration
|
modular design
twin-spool
|
|
gptkbp:engine_power
|
high reliability
high efficiency
superior performance
|
|
gptkbp:engine_thrust_output
|
up to 35,000 lbf
|
|
gptkbp:engine_thrust_vectoring_capability
|
yes
|
|
gptkbp:engine_type
|
high bypass turbofan
F119-PW-400 E
|
|
gptkbp:fan_art
|
wide-chord fan
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
1,360 kg
5.03 m
1.02 m
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-400
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:operational_range
|
1,839 miles
|
|
gptkbp:operational_use
|
gptkb:2005
|
|
gptkbp:propulsion
|
yes
11.67:1
35,000 lbf
156 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|