gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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gptkb:BAE_Systems_Hawk
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gptkbp:application
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military training aircraft
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gptkbp:diameter
|
0.9 m
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gptkbp:displacement
|
significant impact on military aviation.
|
gptkbp:engine
|
used in various aircraft types
low bypass ratio
legacy continues in modern designs
|
gptkbp:engineConfiguration
|
turbojet engine
produced in large numbers
developed_in_the_UK
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gptkbp:engineType
|
axial compressor
single-stage turbine
advanced features for its time
multiple variants exist
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
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gptkbp:hasArea
|
extensively tested
certified by various aviation authorities
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 209
|
gptkbp:introduced
|
1970s
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
gptkbp:length
|
1.8 m
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
gptkbp:noise_level
|
low noise emissions
|
gptkbp:notableUsers
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Kuwait_Air_Force
gptkb:Singapore_Air_Force
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
gptkb:Oman_Air_Force
gptkb:Malaysia_Air_Force
|
gptkbp:operationalHistory
|
part of a long lineage of engines
|
gptkbp:performances
|
modular design
high reliability
high thrust-to-weight ratio
detailed specifications available
fuel efficient
|
gptkbp:propulsion
|
20 kN
|
gptkbp:related_engine
|
Brayton_cycle
|
gptkbp:successor
|
gptkb:Adour_Mk_871
|
gptkbp:type
|
turbofan engine
|
gptkbp:updates
|
various upgrades available
|
gptkbp:weight
|
approximately 200 kg
|