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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
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|
gptkbp:design
|
low bypass ratio
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gptkbp:developer
|
jointly_developed_by_Rolls-Royce_and_Turbomeca
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gptkbp:diameter
|
approximately 0.9 m
|
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gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
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gptkbp:engineConfiguration
|
twin-spool
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gptkbp:engineType
|
axial compressor
single-stage turbine
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|
gptkbp:fuel_capacity
|
approximately 0.5 kg/s
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 171-39
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|
gptkbp:introduced
|
1970s
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gptkbp:is_used_in
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gptkb:Hawker_Siddeley_Hawk
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gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:maintenance
|
approximately 1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise operation
|
|
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 and light attack missions
|
|
gptkbp:propulsion
|
approximately 3,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_216
gptkb:Adour_Mk_206
gptkb:Adour_Mk_225
gptkb:Adour_Mk_230
gptkb:Adour_Mk_213
gptkb:Adour_Mk_151
gptkb:Adour_Mk_207
gptkb:Adour_Mk_205
gptkb:Adour_Mk_235
gptkb:Adour_Mk_218
gptkb:Adour_Mk_221
gptkb:Adour_Mk_211
gptkb:Adour_Mk_227
gptkb:Adour_Mk_228
gptkb:Adour_Mk_229
gptkb:Adour_Mk_204
gptkb:Adour_Mk_208
gptkb:Adour_Mk_236
gptkb:Adour_Mk_171
gptkb:Adour_Mk_222
gptkb:Adour_Mk_217
gptkb:Adour_Mk_231
gptkb:Adour_Mk_181
gptkb:Adour_Mk_214
gptkb:Adour_Mk_226
gptkb:Adour_Mk_233
gptkb:Adour_Mk_212
gptkb:Adour_Mk_234
gptkb:Adour_Mk_224
gptkb:Adour_Mk_210
gptkb:Adour_Mk_215
gptkb:Adour_Mk_240
gptkb:Adour_Mk_209
gptkb:Adour_Mk_203
gptkb:Adour_Mk_202
gptkb:Adour_Mk_220
gptkb:Adour_Mk_223
gptkb:Adour_Mk_232
gptkb:Adour_Mk_219
gptkb:Adour_Mk_239
gptkb:Adour_Mk_237
gptkb:Adour_Mk_238
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 400 lb
|