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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:BAE_Systems_Hawk
|
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gptkbp:application
|
military training aircraft
|
|
gptkbp:climate
|
up to 1,000 °C
|
|
gptkbp:controls
|
air start
FADEC
|
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gptkbp:coolingSystem
|
air-cooled
|
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gptkbp:diameter
|
0.9 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
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gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
turbojet
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial
single stage
Adour_Mk_171-5C-1
Adour_Mk_171-5C-10
Adour_Mk_171-5C-2
Adour_Mk_171-5C-3
Adour_Mk_171-5C-4
Adour_Mk_171-5C-5
Adour_Mk_171-5C-6
Adour_Mk_171-5C-7
Adour_Mk_171-5C-8
Adour_Mk_171-5C-9
|
|
gptkbp:fuel_capacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-5C
|
|
gptkbp:inspiration
|
subsonic flight
|
|
gptkbp:introduced
|
1980s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
75 dB
|
|
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:operational_status
|
training missions
|
|
gptkbp:performances
|
3,000 hours
|
|
gptkbp:propulsion
|
23:1
3,500 lbf
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
150 kg
|