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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
|
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:design
|
approximately 5,000 hours
|
|
gptkbp:design_feature
|
modular design
|
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gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
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gptkbp:engineConfiguration
|
twin-spool configuration
|
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gptkbp:engineType
|
gptkb:Adour_Mk_171-40D
gptkb:Adour_Mk_171-40G
gptkb:Adour_Mk_171-40C
gptkb:Adour_Mk_171-40E
gptkb:Adour_Mk_171-40B
gptkb:Adour_Mk_171
gptkb:Adour_Mk_171-40F
gptkb:Adour_Mk_171-40H
gptkb:Adour_Mk_171-40J
gptkb:Adour_Mk_171-40A
axial compressor
air start
axial turbine
Adour Mk 171-40I
|
|
gptkbp:fanBase
|
single-spool fan
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.8 lb/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:historicalEvent
|
derived_from_the_Adour_Mk_151
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-40
|
|
gptkbp:introduced
|
1970s
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
low maintenance requirements
approximately 1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise engine
|
|
gptkbp:notableUsers
|
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
in service
|
|
gptkbp:operationalRange
|
long operational range
|
|
gptkbp:propulsion
|
high power-to-weight ratio
2.92
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
approximately 40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 1,200 lb
|