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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:Hawker_Siddeley_4000
gptkb:Hawker_Siddeley_7000
gptkb:BAE_Systems_146
gptkb:Hawker_Siddeley_3000
gptkb:Hawker_Siddeley_800
gptkb:Hawker_Siddeley_11000
gptkb:Hawker_Siddeley_125
gptkb:Hawker_Siddeley_1000
gptkb:Hawker_Siddeley_23000
gptkb:Hawker_Siddeley_20000
gptkb:Hawker_Siddeley_6000
gptkb:Hawker_Siddeley_14000
gptkb:Hawker_Siddeley_25000
gptkb:Hawker_Siddeley_26000
gptkb:Hawker_Siddeley_15000
gptkb:Hawker_Siddeley_28000
gptkb:BAE_Systems_Hawk
gptkb:Hawker_Siddeley_5000
gptkb:Hawker_Siddeley_22000
gptkb:Hawker_Siddeley_18000
gptkb:Hawker_Siddeley_12000
gptkb:Hawker_Siddeley_21000
gptkb:Hawker_Siddeley_10000
gptkb:Hawker_Siddeley_29000
gptkb:Hawker_Siddeley_2000
gptkb:Hawker_Siddeley_24000
gptkb:Hawker_Siddeley_9000
gptkb:Hawker_Siddeley_19000
gptkb:Hawker_Siddeley_30000
gptkb:BAE_Systems_Avro_RJ
gptkb:Hawker_Siddeley_8000
gptkb:Hawker_Siddeley_16000
Hawker Siddeley 27000
Hawker_Siddeley_13000
Hawker_Siddeley_17000
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gptkbp:application
|
military training aircraft
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gptkbp:coolingSystem
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air-cooled
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gptkbp:design
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low bypass ratio
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gptkbp:developer
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Rolls-Royce_and_Turbomeca
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gptkbp:diameter
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approximately 0.9 m
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gptkbp:engineConfiguration
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twin-spool
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gptkbp:engineType
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axial
single stage
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gptkbp:fuel_capacity
|
0.8 lb/hp/hr
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gptkbp:fuelType
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gptkb:Jet_A-1
annular
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|
https://www.w3.org/2000/01/rdf-schema#label
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Adour Mk 48000
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gptkbp:introduced
|
1970s
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gptkbp:is_used_in
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gptkb:Hawker_Siddeley_Hawk
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gptkbp:length
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approximately 1.5 m
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gptkbp:manufacturer
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gptkb:Rolls-Royce
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gptkbp:notableUsers
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gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
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gptkbp:number_of_stages
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8
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gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:propulsion
|
approximately 4,000 lbf
|
|
gptkbp:related_engine
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gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
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gptkbp:successor
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gptkb:Adour_Mk_871
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gptkbp:type
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turbofan engine
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gptkbp:weight
|
approximately 1,000 lb
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