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gptkbp:instanceOf
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jet engine
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gptkbp:application
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military training aircraft
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
approximately 0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
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gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
axial
single-stage high-pressure turbine
|
|
gptkbp:fuel_capacity
|
0.8 kg/s at full power
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
gptkbp:historicalEvent
|
derived_from_Adour_Mk_871
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31L4
|
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gptkbp:inspiration
|
training and light attack
|
|
gptkbp:introduced
|
1970s
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
1,000 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
|
10
|
|
gptkbp:operational_status
|
in various air forces worldwide
|
|
gptkbp:operationalRange
|
up to 90% of maximum thrust
|
|
gptkbp:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871-31L5
gptkb:Adour_Mk_871
gptkb:Adour_Mk_871-31L3
Brayton_cycle
|
|
gptkbp:reviews
|
high reliability
|
|
gptkbp:services
|
up to 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 lb
|