Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
heavy-lift helicopters
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:firstFlight |
1960
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soloviev D-25V
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
5,500 shp
4,100 kW |
| gptkbp:status |
in service
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Mil_Mi-10
gptkb:Mil_Mi-6 gptkb:Mil_Mi-10K gptkb:Mil_V-12 |
| gptkbp:bfsParent |
gptkb:Mil_Mi-10
|
| gptkbp:bfsLayer |
6
|