|
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:firstRace
|
1970s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:hasDepartment
|
no
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-31L16
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 1.5 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:number_of_stages
|
8 stages
|
|
gptkbp:operational_status
|
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:propulsion
|
approximately 3,500 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_871-31L11
gptkb:Adour_Mk_871-31L6
gptkb:Adour_Mk_871-31L1
gptkb:Adour_Mk_871-31L4
gptkb:Adour_Mk_871-31L14
gptkb:Adour_Mk_871-31L9
gptkb:Adour_Mk_871-31L15
gptkb:Adour_Mk_871-31L5
gptkb:Adour_Mk_871
gptkb:Adour_Mk_871-31L10
gptkb:Adour_Mk_871-31L3
gptkb:Adour_Mk_871-31L7
gptkb:Adour_Mk_871-31L2
gptkb:Adour_Mk_871-31L8
gptkb:Adour_Mk_871-31L13
gptkb:Adour_Mk_871-31L12
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 1,200 lb
|