Thielert Centurion 2.0 diesel
GPTKB entity
Statements (16)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:basedOn |
Mercedes-Benz OM640 engine
|
| gptkbp:configuration |
inline-4
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Germany
|
| gptkbp:displacement |
1991 cc
|
| gptkbp:firstFlight |
2002
|
| gptkbp:fuelType |
gptkb:Jet_A-1
diesel |
| https://www.w3.org/2000/01/rdf-schema#label |
Thielert Centurion 2.0 diesel
|
| gptkbp:manufacturer |
gptkb:Thielert_Aircraft_Engines
|
| gptkbp:powerOutput |
135 hp
|
| gptkbp:successor |
Centurion 2.0s
|
| gptkbp:bfsParent |
gptkb:Gray_Eagle_Extended_Range
|
| gptkbp:bfsLayer |
7
|