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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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trainer aircraft
compatible with various aircraft
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gptkbp:application
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military training aircraft
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gptkbp:controls
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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
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gptkb:Rolls-Royce
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gptkbp:developer
|
joint venture
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gptkbp:diameter
|
0.9 m
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gptkbp:emissionsStandard
|
low emissions
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gptkbp:energyEfficiency
|
high fuel efficiency
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gptkbp:engine
|
air start
pylon-mounted
lightweight engine
efficient cooling system
high thrust output
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gptkbp:engineConfiguration
|
twin-spool
twin-spool design
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gptkbp:engineDisplacement
|
ongoing development efforts
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gptkbp:engineType
|
afterburning turbofan
easy maintenance
axial compressor
single-stage turbine
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gptkbp:firstIntroduced
|
1970s
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
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gptkbp:hasArea
|
extensive testing conducted
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|
gptkbp:hasContent
|
0.8 lb/hp/hr
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gptkbp:historicalEvent
|
developed_from_the_Adour_Mk_1000
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|
https://www.w3.org/2000/01/rdf-schema#label
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Adour Mk 37000
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gptkbp:length
|
1.5 m
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gptkbp:maintenance
|
1,000 hours
|
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gptkbp:maxSpeed
|
Mach_0.9
|
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gptkbp:noise_level
|
low noise
|
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gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
|
|
gptkbp:operationalArea
|
used in training and light attack roles
|
|
gptkbp:operationalRange
|
1,500 km
|
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gptkbp:performance
|
high performance
|
|
gptkbp:performances
|
long engine life
|
|
gptkbp:propulsion
|
0.12
approximately 3,700 lbf
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
|
|
gptkbp:reliability
|
high reliability
|
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gptkbp:retirementYear
|
still in service
|
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gptkbp:services
|
1976
|
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gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 300 kg
|