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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:certifications
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EASA_certified
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gptkbp:constructionMaterial
|
lightweight alloys
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gptkbp:controls
|
air start
digital control system
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gptkbp:coolingSystem
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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
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gptkbp:engineType
|
axial compressor
axial turbine
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gptkbp:fanBase
|
centrifugal fan
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gptkbp:fuel_capacity
|
high fuel efficiency
0.8 kg/kN/h
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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gptkbp:historicalEvent
|
developed_from_Adour_Mk_100
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 40000
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gptkbp:internationalRelations
|
gptkb:Australia
gptkb:India
gptkb:Malaysia
gptkb:Saudi_Arabia
gptkb:Singapore
gptkb:South_Africa
gptkb:United_Kingdom
gptkb:United_States
Indonesia
|
|
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
|
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gptkbp:market_segment
|
military aviation
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise design
|
|
gptkbp:number_of_stages
|
single stage
|
|
gptkbp:operational_status
|
multi-role capability
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:propulsion
|
10:1
4000 lbf
|
|
gptkbp:providesServices
|
global support network
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
upgradable to Mk 951
|
|
gptkbp:weight
|
approximately 400 kg
|