|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:bypassRatio
|
1.15:1
|
|
gptkbp:category
|
gptkb:Rolls-Royce_aircraft_engines
Aerospace engineering
Turbofan engines
Turbomeca aircraft engines
|
|
gptkbp:combustors
|
annular
|
|
gptkbp:compressionRatio
|
two-spool axial
|
|
gptkbp:countryOfOrigin
|
gptkb:France
gptkb:United_Kingdom
|
|
gptkbp:developedBy
|
gptkb:SEPECAT_Jaguar
|
|
gptkbp:diameter
|
0.61 m
|
|
gptkbp:firstRun
|
1968
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Adour
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:length
|
2.9 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
gptkb:Turbomeca
|
|
gptkbp:maximumSpeed
|
24.5 kN
|
|
gptkbp:maximumThrustWithAfterburner
|
32.5 kN
|
|
gptkbp:numberOfStages
|
two
|
|
gptkbp:type
|
turbofan
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
gptkb:United_States_Navy
gptkb:French_Air_Force
gptkb:Indian_Air_Force
|
|
gptkbp:usedInAircraft
|
gptkb:BAE_Hawk
gptkb:McDonnell_Douglas_T-45_Goshawk
gptkb:SEPECAT_Jaguar
gptkb:HAL_Tejas
|
|
gptkbp:variant
|
gptkb:Adour_Mk_101
gptkb:Adour_Mk_102
gptkb:Adour_Mk_104
gptkb:Adour_Mk_106
gptkb:Adour_Mk_151
gptkb:Adour_Mk_871
|
|
gptkbp:weight
|
715 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Holdings
|
|
gptkbp:bfsLayer
|
5
|