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gptkbp:instanceOf
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jet engine
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gptkbp:aircraft
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various trainer aircraft
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gptkbp:application
|
military training aircraft
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gptkbp:atmosphere
|
variable area intake
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gptkbp:climate
|
up to 1,000 °C
|
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
starter motor
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gptkbp:coolingSystem
|
air-cooled
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gptkbp:design_feature
|
modular design
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gptkbp:developer
|
developed_from_Adour_Mk_871
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gptkbp:diameter
|
approximately 2.5 ft
|
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gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
pylon-mounted
|
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gptkbp:engineConfiguration
|
twin-spool
|
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gptkbp:engineType
|
two-stage turbine
multi-stage axial compressor
Mk 871-50E-3 variant
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gptkbp:exhaustSystem
|
convergent-divergent nozzle
|
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gptkbp:fanBase
|
single-stage fan
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
approximately 0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
axial flow
|
|
gptkbp:historicalEvent
|
developed in the 1970s
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Adour Mk 871-50E-3
|
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gptkbp:inspiration
|
gptkb:United_Kingdom
|
|
gptkbp:introduced
|
1980s
|
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gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Hawk
|
|
gptkbp:length
|
approximately 3.5 ft
|
|
gptkbp:maintenance
|
approximately 1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise output
|
|
gptkbp:notableUsers
|
gptkb:Indian_Air_Force
gptkb:Royal_Air_Force
gptkb:Royal_Australian_Air_Force
gptkb:South_African_Air_Force
gptkb:Saudi_Arabian_Air_Force
|
|
gptkbp:operational_status
|
training and light attack missions
|
|
gptkbp:operationalRange
|
up to 40,000 ft
|
|
gptkbp:propulsion
|
4.17:1
approximately 5,000 lbf
|
|
gptkbp:related_engine
|
gptkb:Adour_Mk_951
gptkb:Adour_Mk_871
Adour_family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:services
|
approximately 5,000 hours
|
|
gptkbp:successor
|
gptkb:Adour_Mk_951
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
approximately 1,200 lb
|