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gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:Hawk_T1
|
|
gptkbp:application
|
trainer aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engine
|
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
turbojet engine
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1970s
|
|
gptkbp:fuelCapacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark ignition
afterburning
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-41
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maxSpeed
|
1,200 km/h
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:numberOfStudents
|
single-stage
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:productionCompany
|
1960s to 1970s
|
|
gptkbp:propulsion
|
2.92
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_151
|
|
gptkbp:services
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
military aircraft engine
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
approximately 1,200 lb
|