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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:Hawk_Mk_132
gptkb:Hawk_Mk_128
gptkb:Hawk_Mk_127
gptkb:BAE_Systems_Hawk
gptkb:Hawk_Mk_115
BAE Hawk 100
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|
gptkbp:application
|
military training aircraft
|
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gptkbp:controls
|
digital electronic control
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:diameter
|
approximately 0.9 m
|
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gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-110D
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
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gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
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:operationalRange
|
up to 30,000 ft
|
|
gptkbp:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
gptkb:Adour_Mk_871-31K-110G
gptkb:Adour_Mk_871-31K-110F
Adour Mk 871-31K-110E
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 lb
|