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gptkbp:instanceOf
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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
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gptkbp:design
|
modular design
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gptkbp:designedBy
|
gptkb:Rolls-Royce
|
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gptkbp:diameter
|
0.9 m
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|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
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gptkbp:engine
|
starter motor
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gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
axial compressor
single-stage turbine
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|
gptkbp:environmentalImpact
|
designed to minimize environmental impact
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|
gptkbp:firstIntroduced
|
1970s
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gptkbp:fuelCapacity
|
0.8 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
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|
gptkbp:future_plans
|
potential upgrades planned
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|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 25000
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_plc
|
|
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:numberOfStudents
|
8
|
|
gptkbp:operationalArea
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 30,000 feet
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:performance
|
high performance for training aircraft
|
|
gptkbp:performances
|
approximately 5,000 hours
|
|
gptkbp:propulsion
|
25 kN
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_106
gptkb:Adour_Mk_200
gptkb:Adour_Mk_951
gptkb:Adour_Mk_300
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:serviceHistory
|
used by several air forces
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:supports
|
ground support equipment required
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 200 kg
|