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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_type
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gptkb:fighter_aircraft
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:check_in_time
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equipped with afterburner
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gptkbp:combustor_type
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annular combustion chamber
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gptkbp:compressor_type
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axial compressor
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gptkbp:control_system
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digital electronic control
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gptkbp:cooling_system
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air-cooled
efficient cooling system
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gptkbp:design
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designed for high performance
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gptkbp:development
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developed in the 1970s
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gptkbp:diameter
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1.2 m
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gptkbp:elevation
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up to 50,000 ft
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gptkbp:emissions_standard
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low emissions
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gptkbp:engine
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gptkb:advanced_technology
air start
multiple advanced features
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gptkbp:engine_configuration
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pylon-mounted
twin-engine configuration
detailed specifications available
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gptkbp:engine_power
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high power output
excellent performance
up to 4,000 hours
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gptkbp:engine_type
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military turbofan engine
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gptkbp:fan_art
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single-stage fan
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gptkbp:first_flight
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gptkb:1972
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gptkbp:fuel_capacity
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lightweight design
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gptkbp:fuel_economy
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high fuel efficiency
0.8 lb/hp/hr
low fuel consumption
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gptkbp:fuel_type
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gptkb:Jet_A-1
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|
https://www.w3.org/2000/01/rdf-schema#label
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M53-P38 engine
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gptkbp:investment
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high pressure
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gptkbp:is_tested_for
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extensively tested
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gptkbp:length
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3.8 m
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gptkbp:maintenance
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1,500 hours
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gptkbp:manufacturer
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gptkb:General_Electric
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gptkbp:noise_level
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low noise
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gptkbp:operational_range
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long operating range
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gptkbp:predecessor
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M53-P2 engine
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gptkbp:propulsion
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20:1
25,000 lbf
not equipped
not equipped with thrust reverser
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gptkbp:related_aircraft
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compatible with multiple aircraft
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gptkbp:reliability
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high reliability
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gptkbp:service_entry
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gptkb:1974
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gptkbp:successor
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gptkb:F110-GE-100
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gptkbp:turbine_type
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high bypass turbine
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gptkbp:type
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gptkb:turbofan_engine
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gptkbp:used_in
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gptkb:Mc_Donnell_Douglas_F-15_Eagle
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gptkbp:weight
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1,200 kg
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gptkbp:bfsParent
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gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
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gptkbp:bfsLayer
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6
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