|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combat_radius
|
1,839 km
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
air-cooled system
|
|
gptkbp:design
|
modular
|
|
gptkbp:development
|
YF119
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
3.0 ft
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:advanced_technology
ongoing improvements
|
|
gptkbp:engine_configuration
|
twin-engine
|
|
gptkbp:engine_power
|
high efficiency
superior performance
26,000 lbf without afterburner
|
|
gptkbp:engine_power_afterburner
|
35,000 lbf with afterburner
|
|
gptkbp:engine_type
|
gptkb:F119-PW-100
high bypass turbofan
|
|
gptkbp:features
|
thrust vectoring
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
4.9 m
0.91 m
1,270 kg
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-GE-100 engine
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
16.5 ft
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.25
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operational_use
|
air superiority
|
|
gptkbp:primary_user
|
gptkb:United_States_Air_Force
|
|
gptkbp:propulsion
|
12.5:1
35,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:F-22_family
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:2005
|
|
gptkbp:testbed_aircraft
|
gptkb:YF-22
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Martin_F-22_Raptor
|
|
gptkbp:weight
|
2,800 lb
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation_Operations
|
|
gptkbp:bfsLayer
|
6
|