|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
advanced jet trainer
military training aircraft
|
|
gptkbp:controls
|
FADEC
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular construction
training and light attack
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:energyEfficiency
|
high
|
|
gptkbp:engine
|
rear-mounted
air start
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
turbojet
axial
single-stage
|
|
gptkbp:fanBase
|
centrifugal
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:hasDepartment
|
no
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_101
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 239
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:market
|
available
|
|
gptkbp:maximumDepth
|
1,000 °C
|
|
gptkbp:noise_level
|
low
|
|
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:numberOfStudents
|
8
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:performances
|
3,000 hours
|
|
gptkbp:productionCompany
|
in production
|
|
gptkbp:propulsion
|
14:1
3,500 lbf
|
|
gptkbp:regulatoryCompliance
|
EASA_certified
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
250 kg
|