gptkbp:instanceOf
|
jet engine
|
gptkbp:aircraft
|
Hawk_family
|
gptkbp:application
|
military training aircraft
|
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 26000
|
gptkbp:introduced
|
1970s
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:length
|
approximately 1.5 m
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:notable_feature
|
modular design
ease of maintenance
reliable performance
low bypass ratio
|
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:Kuwaiti_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
gptkbp:propulsion
|
approximately 20 kN
|
gptkbp:related_engine
|
gptkb:Adour_Mk_4000
gptkb:Adour_Mk_5000
gptkb:Adour_Mk_3000
gptkb:Adour_Mk_951
gptkb:Adour_Mk_8000
gptkb:Adour_Mk_1500
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_2000
gptkb:Adour_Mk_9000
gptkb:Adour_Mk_871
gptkb:Adour_Mk_7000
Adour Mk 6000
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
gptkbp:type
|
turbofan engine
|
gptkbp:weight
|
approximately 200 kg
|