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gptkbp:instanceOf
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turbofan engine
|
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gptkbp:aircraft
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gptkb:BAE_Hawk_200
gptkb:Hawker_Siddeley_HS.125
gptkb:Hawker_Siddeley_Harrier
gptkb:Hawker_Siddeley_Buccaneer
gptkb:BAE_Systems_Hawk
gptkb:Hawker_Siddeley_Nimrod
gptkb:Hawker_Siddeley_HS.748
gptkb:BAE_Hawk_T1
BAE Hawk 100
BAE Hawk T2
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gptkbp:application
|
trainer aircraft
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
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gptkbp:developer
|
gptkb:joint_venture_between_Rolls-Royce_and_British_Aerospace
|
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gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
low emissions
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gptkbp:engineType
|
axial
|
|
gptkbp:fanBase
|
single-stage fan
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gptkbp:firstFlight
|
1974
|
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gptkbp:fuel_capacity
|
0.8 lb/hp/hr
|
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gptkbp:fuelType
|
gptkb:Jet_A-1
annular
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 400
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
modular design
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
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gptkbp:noise_level
|
low noise
|
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gptkbp:operational_status
|
gptkb:United_Arab_Emirates_Air_Force
gptkb:Indian_Air_Force
gptkb:Qatar_Emiri_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:Royal_Navy
gptkb:Kuwaiti_Air_Force
gptkb:Omani_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:propulsion
|
4000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_1000
gptkb:Adour_Mk_871
Brayton_cycle
|
|
gptkbp:services
|
approximately 4000 hours
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
military engine
|
|
gptkbp:weight
|
approximately 400 kg
|