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gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:check_in_time
|
gptkb:battle
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
5,000 hours
|
|
gptkbp:developer
|
$1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
twin-engine
twin-spool
air start
pylon-mounted
|
|
gptkbp:engine_type
|
axial compressor
military turbofan
high bypass turbine
|
|
gptkbp:first_flight
|
gptkb:1972
|
|
gptkbp:fuel_capacity
|
high
1.2 m
1,200 kg
3.8 m
0.85 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M53-P42 engine
|
|
gptkbp:is_tested_for
|
gptkb:NASA_Glenn_Research_Center
|
|
gptkbp:launch_date
|
30 seconds
|
|
gptkbp:length
|
3.8 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:max_speed
|
Mach 2.5
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_range
|
2,500 miles
|
|
gptkbp:predecessor
|
gptkb:J79_engine
|
|
gptkbp:produced_by
|
1,500 units
|
|
gptkbp:production_years
|
gptkb:1970
gptkb:1990
|
|
gptkbp:propulsion
|
gptkb:battle
18:1
22,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
60,000 ft
|
|
gptkbp:successor
|
gptkb:F119_engine
|
|
gptkbp:technology
|
supercruise
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
gptkb:Mc_Donnell_Douglas_F-15_Eagle
|
|
gptkbp:water_source
|
1,200 lb/hr
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
gptkb:Snecma_Moteurs
|
|
gptkbp:bfsLayer
|
5
|