gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:Bae_Hawk
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gptkbp:application
|
military training aircraft
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:design_feature
|
modular design
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gptkbp:developer
|
gptkb:Adour_engine_family
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gptkbp:diameter
|
approximately 0.9 m
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
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gptkbp:engine
|
used in various trainer aircraft.
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gptkbp:engineConfiguration
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twin-spool
|
gptkbp:engineType
|
afterburning turbofan
axial compressor
air start
single-stage turbine
advanced materials used
Adour_Mk_871-31K-110L_variant
|
gptkbp:fanBase
|
single-stage fan
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.8 lb/hp/hr
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
dual fuel system
|
gptkbp:hasArea
|
extensive ground testing
certified by various aviation authorities
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-110L
|
gptkbp:introduced
|
1970s
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:length
|
approximately 1.5 m
|
gptkbp:maintenance
|
approximately 1,500 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:noise_level
|
low noise output
|
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:operationalHistory
|
used in various air forces worldwide
|
gptkbp:operationalRange
|
up to 30,000 feet
|
gptkbp:performances
|
approximately 5,000 hours
optimized for training missions
scheduled overhaul every 2,500 hours
|
gptkbp:propulsion
|
no thrust vectoring
11.67
approximately 3,500 lbf
|
gptkbp:related_engine
|
Brayton_cycle
|
gptkbp:reliability
|
high reliability
|
gptkbp:service_ceiling
|
40,000 feet
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
gptkbp:type
|
turbofan engine
|
gptkbp:updates
|
upgraded versions available
|
gptkbp:weight
|
approximately 300 kg
|