|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
trainer aircraft
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
|
|
gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:fuel_capacity
|
0.8 lb/lbf/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:historicalEvent
|
derived_from_the_Rolls-Royce_Spey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 8000
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 3.5 ft
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:operationalRange
|
up to 30,000 ft
|
|
gptkbp:propulsion
|
approximately 5,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
military engine
|
|
gptkbp:weight
|
approximately 1,200 lb
|