|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:climate
|
-40 to 50 °C
|
|
gptkbp:compressionRatio
|
16:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
intercooler
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:duration
|
1,000 hours
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_4
|
|
gptkbp:engine
|
gptkb:Seville,_Spain
modular design
military transport aircraft
|
|
gptkbp:engineConfiguration
|
development phase
twin-engine
|
|
gptkbp:engineType
|
gptkb:TP400-D6A
6
turboprop
high-pressure turbine
air start
|
|
gptkbp:firstFlight
|
2009
|
|
gptkbp:firstRace
|
2005
|
|
gptkbp:fuel_capacity
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
annular combustor
|
|
gptkbp:hasArea
|
EASA_certified
Istanbul,_Turkey
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TP400-D6 turboprop engines
|
|
gptkbp:is_used_in
|
gptkb:Airbus_A400M_Atlas
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Europrop_International
|
|
gptkbp:maximum_speed
|
400 knots
|
|
gptkbp:noise_level
|
75 dB
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:operationalRange
|
8,700 km
|
|
gptkbp:performances
|
high
excellent
20,000 hours
|
|
gptkbp:powerOutput
|
11,000 shp
|
|
gptkbp:propulsion
|
4.5 m
5,000 lbf
4.2:1
variable-pitch propeller
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:type
|
four-shaft engine
|
|
gptkbp:updates
|
TP400-D6B
|
|
gptkbp:weight
|
1,200 kg
|