|
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:developer
|
joint_venture_between_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:energyEfficiency
|
high fuel efficiency
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-46
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:UAE_Air_Force
gptkb:United_Arab_Emirates_Air_Force
gptkb:Egyptian_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Philippine_Air_Force
gptkb:Singapore_Air_Force
gptkb:Bangladesh_Air_Force
gptkb:Qatar_Air_Force
gptkb:Indian_Air_Force
gptkb:Moroccan_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Bahraini_Air_Force
gptkb:Pakistan_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Jordanian_Air_Force
gptkb:Oman_Air_Force
gptkb:Malaysia_Air_Force
gptkb:New_Zealand_Air_Force
gptkb:Thailand_Air_Force
Indonesia Air Force
|
|
gptkbp:operationalArea
|
military training
|
|
gptkbp:performance
|
high reliability
|
|
gptkbp:propulsion
|
11.67
approximately 3,500 lbf
|
|
gptkbp:relatedTo
|
gptkb:Adour_engine_family
|
|
gptkbp:services
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
military engine
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
approximately 300 kg
|