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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:accessories
|
various engine accessories available
|
|
gptkbp:aircraft
|
gptkb:BAE_Systems_Hawk
|
|
gptkbp:application
|
military training aircraft
|
|
gptkbp:certifications
|
certified by aviation authorities
|
|
gptkbp:constructionMaterial
|
lightweight alloys
|
|
gptkbp:controls
|
air start
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
British_design
|
|
gptkbp:developer
|
joint venture
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
compliant with regulations
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial compressor
single stage turbine
|
|
gptkbp:fuel_capacity
|
moderate
variable
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
dual fuel system
|
|
gptkbp:history
|
developed for advanced trainer aircraft.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 21000
|
|
gptkbp:integration
|
integrated into various platforms
|
|
gptkbp:introduced
|
1970s
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:legacy
|
used in various trainer aircraft
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
low maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market
|
military aviation market
|
|
gptkbp:maximum_speed
|
subsonic speeds
|
|
gptkbp:modifications
|
various upgrades available
|
|
gptkbp:noise_level
|
low noise output
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
|
|
gptkbp:operational_status
|
gptkb:Royal_Air_Force
|
|
gptkbp:operationalRange
|
up to 10,000 m
|
|
gptkbp:performance
|
subsonic
|
|
gptkbp:performances
|
approximately 3,000 hours
|
|
gptkbp:propulsion
|
high
20 kN
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:training
|
pilot training systems
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:updates
|
performance upgrades available
|
|
gptkbp:weight
|
approximately 200 kg
|