|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital control system
FADEC
|
|
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
|
gptkb:Adour_Mk_171-23
1.5 m
advanced materials
military aircraft
400 lb
air start
used in various aircraft models
efficient cooling system
|
|
gptkbp:engineConfiguration
|
gptkb:Rolls-Royce
twin-spool
|
|
gptkbp:engineDisplacement
|
0.9 m
developed in the 1970s
|
|
gptkbp:engineType
|
high reliability
afterburning turbofan
high thrust-to-weight ratio
axial compressor
single-stage turbine
low maintenance requirements
Adour_Mk_151,_Adour_Mk_171
certified_by_UK_authorities
|
|
gptkbp:firstIntroduced
|
1980s
|
|
gptkbp:fuelCapacity
|
approximately 0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasArea
|
extensively tested
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-23
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
approximately 1,000 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalStatus
|
up to 40,000 ft
|
|
gptkbp:propulsion
|
8.75:1
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
Adour_series
|
|
gptkbp:relatedTo
|
gptkb:Rolls-Royce_Spey
|
|
gptkbp:services
|
1980
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 400 lb
|