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gptkbp:instanceOf
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jet engine
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gptkbp:application
|
light attack aircraft
advanced jet trainer
military training aircraft
combat aircraft
|
|
gptkbp:certifications
|
civil and military certification
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
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gptkbp:design
|
modular design
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|
gptkbp:developer
|
Rolls-Royce_and_Turbomeca
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|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:engineType
|
axial
single-stage high-pressure turbine
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|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 951-10
|
|
gptkbp:introduced
|
1980s
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|
gptkbp:is_used_in
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:legacy
|
still in use today
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
low maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
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
|
10 stages
|
|
gptkbp:operationalHistory
|
used in various air forces worldwide
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:performance
|
reliable operation
high thrust-to-weight ratio
good fuel efficiency
|
|
gptkbp:propulsion
|
approximately 4,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951-12
gptkb:Adour_Mk_871
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951-12
|
|
gptkbp:technology
|
engine control systems
jet propulsion technology
turbofan technology
aero-engine technology
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
various upgrades over the years
|
|
gptkbp:weight
|
approximately 400 lb
|