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gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
military transport aircraft
|
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gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
30,000 hours
|
|
gptkbp:designedFor
|
gptkb:Airbus_A400M
|
|
gptkbp:developer
|
European_consortium
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:energyEfficiency
|
high fuel efficiency
|
|
gptkbp:engine
|
1,500 kg
pylon-mounted
automatic start
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
optimized performance
high bypass ratio
two-stage turbine
high bypass turbofan
several variants available
|
|
gptkbp:fanBase
|
wide-chord fan
|
|
gptkbp:firstFlight
|
2005
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
gptkbp:generator
|
1,600 °C
|
|
gptkbp:hasArea
|
extensive ground testing
|
|
gptkbp:hasContent
|
0.5 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TP400-D6A
|
|
gptkbp:launchSite
|
air start
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise emissions
|
|
gptkbp:numberBuilt
|
over 1,000
|
|
gptkbp:operatingHours
|
30:1
|
|
gptkbp:operationalArea
|
military operations
|
|
gptkbp:operationalStatus
|
up to 40,000 feet
|
|
gptkbp:partnerships
|
international collaboration
|
|
gptkbp:propulsion
|
no thrust vectoring
14,000 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:rotorDiameter
|
1,200 mm
|
|
gptkbp:services
|
2009
|
|
gptkbp:setting
|
four-shaft engine
|
|
gptkbp:type
|
turbofan
|
|
gptkbp:weight
|
1,500 kg
|