Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
helicopter engine
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:diameter |
0.48 m
|
| gptkbp:family |
gptkb:Turbomeca_Makila
|
| gptkbp:firstFlight |
1976
|
| gptkbp:fuelType |
gptkb:gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Makila 1A1
|
| gptkbp:length |
1.32 m
|
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:powerOutput |
1,330 kW
1,780 shp |
| gptkbp:status |
in service
|
| gptkbp:type |
twin-shaft turboshaft
|
| gptkbp:usedIn |
gptkb:Eurocopter_AS532_Cougar
gptkb:Eurocopter_AS332_Super_Puma gptkb:Eurocopter_EC225_Super_Puma Denel Oryx |
| gptkbp:weight |
210 kg
|
| gptkbp:bfsParent |
gptkb:AS532_Cougar
gptkb:Aérospatiale_AS332_Super_Puma gptkb:AS332_Super_Puma |
| gptkbp:bfsLayer |
6
|