|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
military training 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
|
0.9 m
|
|
gptkbp:engine
|
low
1.5 m
150 kg
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineDisplacement
|
0.9 m
|
|
gptkbp:engineType
|
high
excellent
axial
single-stage
afterburning turbofan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark ignition
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 1500
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 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
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:numberOfStudents
|
8
|
|
gptkbp:operationalRange
|
2000 km
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:productionCompany
|
production
|
|
gptkbp:propulsion
|
10:1
1500 lbf
|
|
gptkbp:services
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
150 kg
|