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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:BAE_Systems_Hawk
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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 turbine blades
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gptkbp:design
|
low bypass ratio
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gptkbp:design_feature
|
modular design
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gptkbp:developer
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gptkb:joint_venture_between_Rolls-Royce_and_British_Aerospace
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gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant with modern standards
|
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gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
single-stage high-pressure turbine
single-stage low-pressure compressor
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|
gptkbp:fanBase
|
single-stage fan
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gptkbp:fuel_capacity
|
high fuel efficiency
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
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gptkbp:historicalEvent
|
evolved from earlier designs
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 205
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|
gptkbp:introduced
|
1970s
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gptkbp:is_a_subject_of
|
compact size
lightweight construction
high reliability
high thrust-to-weight ratio
easy maintenance
low operational costs
robust design
advanced materials used
suitable for various aircraft types
versatile application
adaptable to different missions
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|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
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gptkbp:market_segment
|
military aviation
|
|
gptkbp:noise_level
|
low noise output
|
|
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:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
varies by aircraft
|
|
gptkbp:propulsion
|
20 kN
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_106
gptkb:Adour_Mk_151
gptkb:Adour_Mk_202
|
|
gptkbp:reviews
|
reliable performance
|
|
gptkbp:services
|
approximately 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|