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gptkbp:instanceOf
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turbofan engine
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|
gptkbp:aircraft
|
Hawk_family
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gptkbp:application
|
military training aircraft
|
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gptkbp:controls
|
digital control system
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:designedFor
|
gptkb:Hawker_Siddeley_Hawk
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gptkbp:diameter
|
1,000 mm
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|
gptkbp:emissionsStandard
|
compliant_with_ICAO_standards
|
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gptkbp:engine
|
lightweight design
low noise
military and civilian applications
rear-mounted
high bypass ratio
advanced jet trainer
detailed specifications available
interstage cooling
air-start
|
|
gptkbp:engineConfiguration
|
twin-spool
twin-spool design
|
|
gptkbp:engineDisplacement
|
ongoing improvements
modern design principles
|
|
gptkbp:enginePower
|
high power output
|
|
gptkbp:engineType
|
gptkb:Adour_Mk_951
high reliability
axial
high efficiency
turbojet engine
high thrust-to-weight ratio
low maintenance requirements
single-stage high-pressure turbine
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelCapacity
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:hasArea
|
extensively tested
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:historicalEvent
|
developed from the Adour Mk 100
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 4700
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:maxSpeed
|
Mach_0.9
|
|
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:numberOfStudents
|
5
|
|
gptkbp:operationalHistory
|
used by several air forces
|
|
gptkbp:producedBy
|
gptkb:Rolls-Royce
|
|
gptkbp:propulsion
|
11.75
4,700 lbf
|
|
gptkbp:services
|
40,000 ft
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:weight
|
400 kg
|