|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
trainer aircraft
light attack aircraft
military trainer
advanced jet trainer
combat aircraft
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
twin-spool
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO
|
|
gptkbp:engineConfiguration
|
turbofan
|
|
gptkbp:engineType
|
axial
high bypass ratio
|
|
gptkbp:fanBase
|
single-stage
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuel_capacity
|
0.8 kg/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 14000
|
|
gptkbp:is_used_in
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_status
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:powerOutput
|
10,000 to 14,000 lbf
|
|
gptkbp:propulsion
|
14,000 lbf
35:1
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_151
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Adour_Mk_151
|
|
gptkbp:training
|
gptkb:Adour_engine_family
|
|
gptkbp:type
|
military engine
|
|
gptkbp:weight
|
400 kg
|