Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine family
|
| gptkbp:engineType |
turboprop
|
| gptkbp:features |
full authority digital engine control (FADEC)
counter-rotating propellers |
| gptkbp:firstFlight |
2009
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:hasModel |
gptkb:Europrop_TP400-D6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Airbus A400M engines
|
| gptkbp:manufacturer |
gptkb:Europrop_International
|
| gptkbp:notable_for |
most powerful turboprop engine in western production
|
| gptkbp:numberOfEnginesPerAircraft |
4
|
| gptkbp:powerOutput |
11,000 shp
|
| gptkbp:propellerBlades |
8
|
| gptkbp:propellerDiameter |
5.33 m
|
| gptkbp:propellerManufacturer |
Ratier-Figeac
|
| gptkbp:usedOn |
gptkb:Airbus_A400M_Atlas
|
| gptkbp:bfsParent |
gptkb:Motoren-_und_Turbinen-Union
|
| gptkbp:bfsLayer |
7
|