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gptkbp:instance_of
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gptkb:turbofan_engine
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|
gptkbp:application
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gptkb:transport_aircraft
|
|
gptkbp:armament
|
gptkb:6
|
|
gptkbp:average_temperature
|
high temperature resistant
|
|
gptkbp:certification
|
EASA certified
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|
gptkbp:combustor_type
|
annular combustor
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|
gptkbp:compression_ratio
|
16:1
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|
gptkbp:compressor_type
|
axial compressor
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|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
Airbus, Rolls-Royce, Safran, MTU Aero Engines
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissions_standard
|
compliant with ICAO standards
|
|
gptkbp:engine_configuration
|
twin-engine layout
|
|
gptkbp:engine_power
|
20,000 flight hours
|
|
gptkbp:exhaust_system
|
mixed flow
|
|
gptkbp:first_flight
|
gptkb:2007
|
|
gptkbp:fuel_economy
|
high efficiency
low fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
electronic fuel control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
gptkbp:has_programs
|
European military transport aircraft program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Europrop TP400-D6
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:launch_date
|
short startup time
|
|
gptkbp:legal_principle
|
turbine engine principle
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
3,000 flight hours
|
|
gptkbp:manufacturer
|
gptkb:Europrop_International
|
|
gptkbp:market_segment
|
gptkb:military_aircraft
|
|
gptkbp:max_speed
|
400 knots
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:number_of_stages
|
10 stages
|
|
gptkbp:operational_range
|
1,000 nautical miles
|
|
gptkbp:original_run
|
gptkb:2005
|
|
gptkbp:power_output
|
8,000 k W
|
|
gptkbp:project
|
ongoing improvements in efficiency and performance
|
|
gptkbp:propeller
|
4.5 m
1,000 RPM
variable pitch propeller
|
|
gptkbp:propulsion
|
high power-to-weight ratio
11,000 lbf
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
37,000 feet
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:type
|
four-shaft engine
|
|
gptkbp:type_of
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Airbus_A400_M_Atlas
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Airbus_A400_M
|
|
gptkbp:bfsLayer
|
5
|