|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
Hawk_family
|
|
gptkbp:application
|
military training
trainer aircraft
|
|
gptkbp:certifications
|
civil certification
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:design
|
modular design
twin-spool
|
|
gptkbp:developer
|
joint venture
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:energyEfficiency
|
high efficiency
|
|
gptkbp:engineType
|
axial compressor
axial turbine
|
|
gptkbp:exportedTo
|
multiple countries
|
|
gptkbp:firstFlight
|
1974
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
dual fuel system
|
|
gptkbp:hasContent
|
0.8 lb/hp/hr
|
|
gptkbp:hasDepartment
|
optional
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 12000
|
|
gptkbp:innovation
|
advanced technology
|
|
gptkbp:launchSite
|
air start
|
|
gptkbp:legacy
|
long legacy in aviation
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:maintenance
|
2000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:numberOfStudents
|
8 stages
|
|
gptkbp:operationalArea
|
used in various air forces
|
|
gptkbp:operationalStatus
|
up to 40,000 ft
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:propulsion
|
24:1
annular
12000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
gptkb:Adour_Mk_871
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:safety
|
high safety standards
|
|
gptkbp:services
|
5000 hours
|
|
gptkbp:status
|
in service
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:type
|
military engine
|
|
gptkbp:updates
|
available upgrades
|
|
gptkbp:usedIn
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:weight
|
approximately 500 kg
|