|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:General_Electric's_aviation_division
|
|
gptkbp:aircraft_operated
|
gptkb:star
air superiority
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:certification
|
military certification
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
advanced cooling system
|
|
gptkbp:design
|
modular design
20,000 hours
|
|
gptkbp:developer
|
gptkb:Joint_Strike_Fighter_program
high
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
twin-engine configuration
|
|
gptkbp:engine_type
|
gptkb:3
2
turbofan
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
high
efficient fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:JP-8
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
F119-PW-800 Engine
|
|
gptkbp:innovation
|
gptkb:advanced_technology
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:launch_date
|
short startup time
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_area
|
combat missions
|
|
gptkbp:part_of
|
gptkb:F-22_program
|
|
gptkbp:performance
|
superior performance
|
|
gptkbp:project
|
ongoing development
|
|
gptkbp:propulsion
|
gptkb:battle
high
high thrust-to-weight ratio
35,000 lbf
8,500 lbf·s/lb
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
gptkb:2005
|
|
gptkbp:supports
|
high airflow
|
|
gptkbp:sustainability
|
sustainable practices
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:F-22_Raptor
|
|
gptkbp:weight
|
1,500 lb
|