|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_type
|
gptkb:stealth_technology
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
24:1
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:elevation
|
up to 65,000 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:military_aircraft
ongoing
advanced materials
modular
state-of-the-art
|
|
gptkbp:engine_configuration
|
twin-spool
high bypass ratio
|
|
gptkbp:engine_power
|
high
6,000 hours
superior
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
|
|
gptkbp:facilities
|
Pratt & Whitney's West Palm Beach facility
|
|
gptkbp:features
|
vectoring thrust
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_capacity
|
1,500 kg
|
|
gptkbp:fuel_economy
|
high
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
gptkbp:has_programs
|
gptkb:Advanced_Tactical_Fighter_(ATF)_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119 engine family
|
|
gptkbp:is_tested_for
|
extensive
|
|
gptkbp:length
|
16 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:military_branch
|
gptkb:United_States_Air_Force
|
|
gptkbp:number_of_stages
|
3 stages
|
|
gptkbp:operational_range
|
1,839 miles
|
|
gptkbp:original_run
|
gptkb:1996
|
|
gptkbp:produced_by
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:propulsion
|
yes
high
variable
35,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-22_Raptor
|
|
gptkbp:successor
|
gptkb:F135_engine_family
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:twin_Pratt_&_Whitney_F119-PW-100
|
|
gptkbp:bfsLayer
|
8
|