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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
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gptkbp:application
|
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:diameter
|
approximately 0.9 m
|
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gptkbp:emissionsStandard
|
low emissions
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gptkbp:engineConfiguration
|
twin-spool configuration
|
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gptkbp:engineType
|
axial compressor
single-stage turbine
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gptkbp:environmental_impact
|
designed for reduced environmental impact
|
|
gptkbp:fanBase
|
single-stage fan
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|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
good fuel efficiency
0.85 kg/kN/h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 901
|
|
gptkbp:inspiration
|
gptkb:United_Kingdom
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:launchSite
|
air start
|
|
gptkbp:length
|
approximately 3.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
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:number_of_stages
|
8 stages
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 10,000 m
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
22 kN
110 kN/t
|
|
gptkbp:related_engine
|
brayton_cycle
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
various upgrades available
|
|
gptkbp:weight
|
approximately 200 kg
|