gptkbp:instanceOf
|
jet engine
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
gptkbp:application
|
military training aircraft
|
gptkbp:controls
|
digital electronic control
|
gptkbp:coolingSystem
|
air-cooled
|
gptkbp:diameter
|
0.9 m
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
gptkbp:engineConfiguration
|
twin-spool
|
gptkbp:engineType
|
axial
single-stage
|
gptkbp:firstRace
|
1964
|
gptkbp:fuel_capacity
|
0.85 kg/kN/h
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 225
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:launchSite
|
air start
|
gptkbp:length
|
1.5 m
|
gptkbp:maintenance
|
200 hours
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:maximum_speed
|
Mach_0.9
|
gptkbp:noise_level
|
low noise
|
gptkbp:operational_status
|
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:Royal_Saudi_Air_Force
gptkb:South_African_Air_Force
|
gptkbp:propulsion
|
22 kN
110 N/kg
|
gptkbp:related_engine
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_171
gptkb:Adour_Mk_901
gptkb:Adour_Mk_202
Adour Mk 1001
Brayton_cycle
Adour_Mk_251
Adour_Mk_301
Adour_Mk_401
Adour_Mk_501
Adour_Mk_601
Adour_Mk_701
Adour_Mk_801
|
gptkbp:service_ceiling
|
12,000 m
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
gptkbp:training
|
gptkb:Adour_engine_family
|
gptkbp:type
|
turbofan engine
|
gptkbp:weight
|
approximately 200 kg
|