Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstFlight |
1981
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca TM 333-2B2
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:numberOfAxles |
1
|
| gptkbp:powerOutput |
825 kW
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedIn |
gptkb:HAL_Cheetal
gptkb:HAL_Dhruv |
| gptkbp:bfsParent |
gptkb:Advanced_Light_Helicopter
|
| gptkbp:bfsLayer |
6
|