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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
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military training aircraft
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gptkbp:controls
|
digital control system
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:design_feature
|
modular design
reliable performance
high thrust-to-weight ratio
easy maintenance
versatile application
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gptkbp:diameter
|
0.9 m
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gptkbp:emissionsStandard
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compliant_with_ICAO_standards
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gptkbp:engineType
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axial compressor
axial turbine
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gptkbp:fanBase
|
single stage fan
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gptkbp:fuel_capacity
|
high efficiency
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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|
gptkbp:future_plans
|
potential for civilian applications
upgraded variants
integration with advanced avionics
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gptkbp:historicalEvent
|
developed_from_Adour_Mk_100
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|
https://www.w3.org/2000/01/rdf-schema#label
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Adour Mk 15000
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gptkbp:introduced
|
1970s
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gptkbp:is_used_in
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gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
military aviation
training aircraft
light combat aircraft
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|
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:number_of_stages
|
3
|
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gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:propulsion
|
37.5
15000 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
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gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 kg
|