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gptkbp:instanceOf
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jet engine
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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
air cooling
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gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
approximately 0.9 m
|
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gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
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gptkbp:engine
|
various military aircraft
inline layout
|
|
gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
turbojet engine
axial compressor
single-stage turbine
multiple variants available
advanced materials used
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 lb/hp/hr
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gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:hasArea
|
extensive testing program
certified_by_EASA
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|
gptkbp:hasDepartment
|
no
|
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gptkbp:historicalEvent
|
derived_from_Adour_Mk_871
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-90C
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
approximately 1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise design
|
|
gptkbp:notable_feature
|
Adour_Mk_871-31K-90C-1
|
|
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:operationalRange
|
varies by aircraft
up to 40,000 ft
|
|
gptkbp:performances
|
high reliability
approximately 5,000 hours
detailed specifications available.
high thrust output
|
|
gptkbp:propulsion
|
8.75:1
approximately 3,500 lbf
|
|
gptkbp:serviceType
|
1976
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
various upgrades available
|
|
gptkbp:weight
|
approximately 400 lb
|