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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
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gptkbp:diameter
|
0.9 m
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gptkbp:engineConfiguration
|
twin-spool
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gptkbp:engineType
|
axial compressor
single-stage turbine
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|
gptkbp:fanBase
|
single-stage fan
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gptkbp:firstFlight
|
1974
|
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gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
spark ignition
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 5000
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
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gptkbp:length
|
1.8 m
|
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gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:operational_status
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Saudi_Air_Force
gptkb:South_African_Air_Force
gptkb:Oman_Air_Force
|
|
gptkbp:propulsion
|
12.5:1
5000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 kg
|