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gptkbp:instanceOf
|
jet engine
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gptkbp:application
|
military training aircraft
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:crew
|
1 pilot
|
|
gptkbp:designedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:developer
|
joint_venture_between_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engine
|
air start
mounted under the wing
|
|
gptkbp:engineConfiguration
|
two-spool
|
|
gptkbp:engineType
|
afterburning turbofan
axial compressor
high-pressure turbine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 23000
|
|
gptkbp:introduced
|
1974
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:maxSpeed
|
1,000 km/h
|
|
gptkbp:operationalArea
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:powerOutput
|
approximately 17.5 kN
|
|
gptkbp:propulsion
|
0.34
23000 lbf
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:relatedTo
|
gptkb:Rolls-Royce_Spey
|
|
gptkbp:replacedBy
|
gptkb:Adour_Mk_951
|
|
gptkbp:services
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedBy
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Nigerian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Malaysian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 500 kg
|