Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:certification |
gptkb:EASA
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:configuration |
four-shaft
|
| gptkbp:constructionStartYear |
2003
|
| gptkbp:countryOfOrigin |
gptkb:Europe
|
| gptkbp:diameter |
2.5 m
|
| gptkbp:firstRun |
2005
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Europrop TP400-D6
|
| gptkbp:length |
3.3 m
|
| gptkbp:manufacturer |
gptkb:Europrop_International
|
| gptkbp:marketedAs |
gptkb:Airbus_A400M
|
| gptkbp:notableFeature |
most powerful turboprop in western production
|
| gptkbp:numberOfAxles |
4
|
| gptkbp:numberOfEngines |
none
|
| gptkbp:partner |
gptkb:Rolls-Royce
gptkb:ITP_Aero gptkb:MTU_Aero_Engines gptkb:Safran_Aircraft_Engines |
| gptkbp:powerOutput |
11,000 shp
|
| gptkbp:propellerBlades |
8
|
| gptkbp:propulsion |
scimitar
|
| gptkbp:usedIn |
gptkb:Airbus_A400M_Atlas
|
| gptkbp:weight |
1,900 kg
|
| gptkbp:bfsParent |
gptkb:A400
gptkb:A400M_military_transport gptkb:A400M gptkb:A400M_military_transport_aircraft |
| gptkbp:bfsLayer |
7
|