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gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military transport aircraft
|
|
gptkbp:certifications
|
EASA_certified
|
|
gptkbp:climate
|
-40 to 50 °C
|
|
gptkbp:collaborations
|
Airbus,_Rolls-Royce,_MTU_Aero_Engines
|
|
gptkbp:constructionMaterial
|
composite materials
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:customerBase
|
international military customers
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engineType
|
6
free turbine
axial compressor
TP400-D6A,_TP400-D6B
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:facilities
|
gptkb:Istanbul_Technical_University
|
|
gptkbp:firstFlight
|
2007
|
|
gptkbp:firstRace
|
2005
|
|
gptkbp:fuel_capacity
|
high efficiency
0.5 lb/hp/hr
high fuel consumption efficiency
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
spark ignition
dual fuel system
|
|
gptkbp:future_plans
|
upgraded versions planned
|
|
gptkbp:hasArea
|
extensive testing program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TP400-D6 engine
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Europrop_International
|
|
gptkbp:market_segment
|
military aviation
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_status
|
low operational cost
in service since 2009
|
|
gptkbp:operationalRange
|
8,700 km
|
|
gptkbp:performances
|
20,000 hours
|
|
gptkbp:powerOutput
|
8,000 kW
|
|
gptkbp:propulsion
|
4
7.33
variable-pitch propeller
11,000 lbf
|
|
gptkbp:related_engine
|
TP400_family
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:supports
|
global support network
|
|
gptkbp:training
|
gptkb:European_Defence_Agency
|
|
gptkbp:type
|
four-shaft turboprop engine
|
|
gptkbp:usedIn
|
gptkb:Airbus_A400M_Atlas
|
|
gptkbp:weight
|
1,500 kg
|