Adour Mk 171-38

GPTKB entity

Statements (81)
Predicate Object
gptkbp:instanceOf jet engine
gptkbp:application military training aircraft
gptkbp:coolingSystem air-cooled
gptkbp:diameter approximately 0.9 m
gptkbp:engineType axial compressor
single-stage turbine
gptkbp:fuelType gptkb:Jet_A-1
annular combustor
https://www.w3.org/2000/01/rdf-schema#label Adour Mk 171-38
gptkbp:introduced 1970s
gptkbp:is_used_in gptkb:Hawker_Siddeley_Hawk
gptkbp:length approximately 1.5 m
gptkbp:manufacturer gptkb:Rolls-Royce
gptkbp:notableUsers gptkb:United_Arab_Emirates_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:Omani_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkbp:number_of_stages 8 stages
gptkbp:operationalRange up to 90% of maximum thrust
gptkbp:propulsion approximately 3,500 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_243
gptkb:Adour_Mk_221
gptkb:Adour_Mk_211
gptkb:Adour_Mk_227
gptkb:Adour_Mk_228
gptkb:Adour_Mk_241
gptkb:Adour_Mk_244
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_246
gptkb:Adour_Mk_217
gptkb:Adour_Mk_231
gptkb:Adour_Mk_248
gptkb:Adour_Mk_181
gptkb:Adour_Mk_214
gptkb:Adour_Mk_226
gptkb:Adour_Mk_233
gptkb:Adour_Mk_212
gptkb:Adour_Mk_242
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_249
gptkb:Adour_Mk_247
gptkb:Adour_Mk_202
gptkb:Adour_Mk_245
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
gptkb:Adour_Mk_250
gptkbp:successor gptkb:Adour_Mk_151
gptkbp:type turbofan engine
gptkbp:weight approximately 300 kg