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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
|
Hawk_family
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gptkbp:application
|
military training aircraft
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:criticalReception
|
around 3.5
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gptkbp:design_feature
|
modular design
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gptkbp:diameter
|
0.9 m
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gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
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gptkbp:engineConfiguration
|
twin-spool
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gptkbp:engineType
|
axial
single-stage high-pressure turbine
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|
gptkbp:firstRace
|
1964
|
|
gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
gptkb:full_authority_digital_engine_control_(FADEC)
annular
spark ignition
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gptkbp:historicalEvent
|
derived from the Adour Mk 100
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4500
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
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:propulsion
|
4500 lbf
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 kg
|