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gptkbp:instanceOf
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jet engine
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
trainer aircraft
military training aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant with modern standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
single-stage high-pressure turbine
single-stage low-pressure compressor
|
|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:firstRace
|
1964
|
|
gptkbp:fuel_capacity
|
high efficiency
0.85 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustion chamber
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey_engine.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 223
|
|
gptkbp:inspiration
|
gptkb:United_Kingdom
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:noise_level
|
low noise
|
|
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:operationalHistory
|
used in various air forces
|
|
gptkbp:operationalRange
|
up to 30,000 feet
|
|
gptkbp:propulsion
|
22 kN
110:1
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871
Adour_family
|
|
gptkbp:successor
|
gptkb:Adour_Mk_871
|
|
gptkbp:training
|
gptkb:British_Aerospace
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|