|
gptkbp:instanceOf
|
engine
|
|
gptkbp:airlines
|
100 kg/s
|
|
gptkbp:application
|
Military Aviation
|
|
gptkbp:compressionRatio
|
25:1
|
|
gptkbp:constructionMaterial
|
Variable Geometry Intake
|
|
gptkbp:controls
|
FADEC
Digital_Engine_Control
|
|
gptkbp:coolingSystem
|
Air-cooled
Water-based_Coolant
|
|
gptkbp:design
|
5,000 hours
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:drivetrain
|
Reduction Gearbox
|
|
gptkbp:emissionsStandard
|
gptkb:EPA_Tier_4
|
|
gptkbp:energyEfficiency
|
High Efficiency
|
|
gptkbp:engine
|
Pylon Mounted
Static Test Stand
|
|
gptkbp:engineConfiguration
|
Twin-Spool
|
|
gptkbp:engineType
|
High-Pressure Turbine
Military Turbofan
|
|
gptkbp:fanBase
|
Single-stage Fan
|
|
gptkbp:firstFlight
|
1972
|
|
gptkbp:fuel_capacity
|
1,200 lb/hr
|
|
gptkbp:fuelType
|
gptkb:Spark_Ignition
Fuel Injection System
Jet A
Annular Combustor
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:hasDepartment
|
Optional
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Honeywell F124-GA-100
|
|
gptkbp:launchDate
|
30 seconds
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:maxSpeed
|
Mach_2.5
|
|
gptkbp:noise_level
|
Low Noise
|
|
gptkbp:numberOfStudents
|
3
|
|
gptkbp:operationalRange
|
High Altitude
|
|
gptkbp:operationalStatus
|
30 psi
1,500 °C
|
|
gptkbp:propulsion
|
No
29,000 lbf
|
|
gptkbp:related_engine
|
Brayton_Cycle
|
|
gptkbp:services
|
50,000 ft
|
|
gptkbp:startsAt
|
Electric Starter
|
|
gptkbp:type
|
gptkb:Turbofan_Engine
|
|
gptkbp:usedIn
|
gptkb:McDonnell_Douglas_F-15_Eagle
|
|
gptkbp:weight
|
0.04
1,200 kg
|