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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
|
air start
digital electronic control
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:design
|
3,000 hours
|
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gptkbp:design_feature
|
modular design
advanced materials
improved fuel efficiency
environmentally friendly design
enhanced reliability
high bypass ratio
reduced radar cross-section
low maintenance requirements
digital engine control system
modular maintenance system
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gptkbp:diameter
|
0.9 m
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gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
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gptkbp:engineType
|
single-stage axial compressor
single-stage axial turbine
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|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:fuel_capacity
|
0.8 kg/kN/h
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey_engine
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 222
|
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gptkbp:introduced
|
1970s
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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:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise design
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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:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:propulsion
|
0.11
22 kN
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_171
gptkb:Adour_Mk_181
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 200 kg
|