|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
air-start
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-2
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:productionCompany
|
1960s to 1970s
|
|
gptkbp:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:relatedTo
|
gptkb:Adour_engine_family
gptkb:Pilatus_Aircraft
gptkb:British_Aerospace
gptkb:Lockheed_Martin
gptkb:McDonnell_Douglas
gptkb:Boeing
gptkb:Hawker_Siddeley
gptkb:Dassault_Aviation
gptkb:Embraer
Alenia Aermacchi
Northrop
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 400 lb
|