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gptkbp:instanceOf
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turbofan engine
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gptkbp:aircraft
|
compatible with multiple airframes
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|
gptkbp:airlines
|
60 kg/s
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gptkbp:application
|
military aircraft
used in various aircraft types
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|
gptkbp:certifications
|
certified for military use
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gptkbp:climate
|
high operating temperature
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:coolingSystem
|
air-cooled
used for turbine cooling
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gptkbp:design
|
designed for supersonic flight
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gptkbp:design_feature
|
advanced design features
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|
gptkbp:developer
|
developed_from_Adour_Mk_100
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|
gptkbp:diameter
|
0.9 m
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|
gptkbp:emissionsStandard
|
compliant with regulations
|
|
gptkbp:engineType
|
single-stage fan
two-stage turbine
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|
gptkbp:exhaustSystem
|
convergent nozzle
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|
gptkbp:exportedTo
|
various countries
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|
gptkbp:firstRace
|
1980s
|
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gptkbp:fuel_capacity
|
high fuel efficiency
optimized fuel consumption
0.85 kg/kN·h
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:future_plans
|
potential future developments
|
|
gptkbp:hasArea
|
extensively tested
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 3300M
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
low maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
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gptkbp:market
|
military aviation market
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:notable_feature
|
gptkb:Adour_Mk_151
|
|
gptkbp:notableUsers
|
gptkb:Royal_Air_Force
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalHistory
|
long operational history
|
|
gptkbp:performance
|
excellent performance
|
|
gptkbp:productionYears
|
1970s to 1980s
|
|
gptkbp:propulsion
|
8.25
3300 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_engine_family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:serviceType
|
1980
|
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gptkbp:successor
|
Adour_Mk_351
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
approximately 400 kg
|