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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:F119-PW-500_Engine
gptkb:F119_family
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|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
air superiority
|
|
gptkbp:developer
|
gptkb:General_Electric_Aviation
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
29,000 lbf
twin-spool
high bypass ratio
air start
pylon-mounted
|
|
gptkbp:engine_type
|
gptkb:3
2
military turbofan
|
|
gptkbp:first_flight
|
gptkb:1976
|
|
gptkbp:fuel_capacity
|
high
1,200 kg
1.1 m
3.8 m
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
GE F120
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
2.5
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
subsonic to supersonic
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:original_run
|
gptkb:1974
|
|
gptkbp:propulsion
|
gptkb:battle
29,000 lbf
24.2
0.95 lb/lbf·h
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:GE_F110
|
|
gptkbp:supports
|
1,000 lb/s
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
|
gptkbp:weight
|
1,200 kg
|