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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)
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gptkbp:coolingSystem
|
air-cooled
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|
gptkbp:design_feature
|
modular design
advanced materials
environmentally friendly design
low weight
high bypass ratio
reliable performance
high thrust-to-weight ratio
easy maintenance
digital control system
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|
gptkbp:developer
|
gptkb:Rolls-Royce_Turbomeca_Adour
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gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
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gptkbp:engineType
|
axial compressor
single-stage turbine
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|
gptkbp:exhaustSystem
|
subsonic air intake
|
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gptkbp:fuel_capacity
|
0.8 kg/kN·h
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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gptkbp:hasDepartment
|
no
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31K-110M
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gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
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gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:operational_status
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:South_African_Air_Force
|
|
gptkbp:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871-31K-120
gptkb:Adour_Mk_871-31K-110
gptkb:Adour_Mk_871
gptkb:Adour_Mk_871-31K-100
Brayton_cycle
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:services
|
3,000 hours
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:variant
|
Adour_Mk_871-31K-110M-1
Adour_Mk_871-31K-110M-2
Adour_Mk_871-31K-110M-3
|
|
gptkbp:weight
|
approximately 300 kg
|