|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:F-35_Lightning_II
|
|
gptkbp:average_temperature
|
1,600 ° F
|
|
gptkbp:bypass_ratio
|
5.0:1
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:designed_for
|
gptkb:F-22_Raptor
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
Nox standard compliant
|
|
gptkbp:engine
|
gptkb:F119_family
gptkb:stealth_technology
F120 engine
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:exhaust_system
|
variable geometry
|
|
gptkbp:features
|
thrust vectoring
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
1.2 m
3.8 m
1,500 lb
|
|
gptkbp:fuel_economy
|
high
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:JP-8
dual fuel system
|
|
gptkbp:has_programs
|
gptkb:Joint_Strike_Fighter
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE F119 engine
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
0 to 100% RPM
|
|
gptkbp:operational_use
|
gptkb:2005
gptkb:US_Air_Force
|
|
gptkbp:propulsion
|
35,000 lbf
|
|
gptkbp:related_aircraft
|
multirole fighter
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:service_ceiling
|
65,000 ft
|
|
gptkbp:thrust_vectoring_angle
|
20 degrees
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:variant
|
gptkb:F119-PW-100
|
|
gptkbp:weight
|
1,500 lb
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation
|
|
gptkbp:bfsLayer
|
4
|