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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:design_feature
|
modular design
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gptkbp:diameter
|
0.9 m
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gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:exportedTo
|
multiple countries
|
|
gptkbp:firstFlight
|
1976
|
|
gptkbp:firstRace
|
1970
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.85 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark ignition
annular combustor
|
|
gptkbp:historicalEvent
|
derived from the Adour Mk 100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 220
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:legacy
|
used in various trainer aircraft.
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:modifications
|
various modifications available
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_status
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Royal_Malaysian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
|
gptkbp:operationalRange
|
extended operational range
|
|
gptkbp:propulsion
|
22 kN
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:supportRole
|
pilot training role
|
|
gptkbp:training
|
ground support equipment available
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|