|
gptkbp:instanceOf
|
gptkb:piston_engine
|
|
gptkbp:afterburningThrust
|
32.5 kN
|
|
gptkbp:category
|
gptkb:piston_engine
military jet engine
|
|
gptkbp:countryOfOrigin
|
gptkb:France
gptkb:United_Kingdom
|
|
gptkbp:developedBy
|
gptkb:SEPECAT_Jaguar
|
|
gptkbp:diameter
|
0.74 m
|
|
gptkbp:firstFlight
|
1968
|
|
gptkbp:firstRun
|
1968
|
|
gptkbp:fuelType
|
aviation kerosene
|
|
gptkbp:length
|
2.51 m
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
gptkb:Turbomeca
|
|
gptkbp:notableFeature
|
modular design
low bypass ratio
afterburning capability (in some variants)
|
|
gptkbp:numberOfStages
|
1 (low pressure), 1 (high pressure)
2 (low pressure), 5 (high pressure)
|
|
gptkbp:partner
|
gptkb:Rolls-Royce_Turbomeca_Limited
|
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
gptkb:United_States_Navy
gptkb:French_Air_Force
gptkb:Indian_Air_Force
|
|
gptkbp:status
|
in service
|
|
gptkbp:thrust
|
24.5 kN
|
|
gptkbp:type
|
turbofan
|
|
gptkbp:usedIn
|
gptkb:McDonnell_Douglas_T-45_Goshawk
gptkb:SEPECAT_Jaguar
gptkb:BAE_Systems_Hawk
gptkb:Mikoyan_MiG-27_(experimental)
|
|
gptkbp:variant
|
gptkb:Adour_Mk_101
gptkb:Adour_Mk_102
gptkb:Adour_Mk_104
gptkb:Adour_Mk_106
gptkb:Adour_Mk_871
gptkb:Adour_Mk_811
gptkb:Adour_Mk_951
|
|
gptkbp:weight
|
715 kg
|
|
gptkbp:bfsParent
|
gptkb:McDonnell_Douglas_T-45_Goshawk
gptkb:CT-155_Hawk
gptkb:BAE_Hawk_209
gptkb:T-45_Goshawk
|
|
gptkbp:bfsLayer
|
7
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Adour
|