|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:controls
|
digital electronic control
|
|
gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:developer
|
joint_venture_between_Rolls-Royce_and_Turbomeca
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
0.8 kg/s
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3900
|
|
gptkbp:lastProduced
|
1976
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
200 hours
|
|
gptkbp:noise_level
|
low noise output
|
|
gptkbp:notableUsers
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
|
|
gptkbp:operationalHistory
|
used by several air forces
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
3900 lbf
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_4000
gptkb:Adour_Mk_5000
gptkb:Adour_Mk_3000
gptkb:Adour_Mk_951
gptkb:Adour_Mk_8000
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_2000
gptkb:Adour_Mk_9000
gptkb:Adour_Mk_7000
Adour Mk 6000
|
|
gptkbp:retirementYear
|
still in service
|
|
gptkbp:services
|
1976
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:totalGoals
|
over 1000 units
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:usedIn
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:weight
|
1500 lb
|