Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
heavy-lift helicopters
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:powerOutput |
4,100 kW
|
| gptkbp:usedInAircraft |
gptkb:Mil_Mi-10
gptkb:Mil_Mi-6 gptkb:Mil_Mi-10K |
| gptkbp:bfsParent |
gptkb:2_×_Soloviev_D-25V_turboshaft
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Soloviev D-25V turboshaft
|