Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
heavy-lift helicopters
|
| gptkbp:compressionRatio |
axial
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soloviev D-25VF
|
| gptkbp:length |
3.95 m
|
| gptkbp:manufacturer |
gptkb:Soloviev_Design_Bureau
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:powerOutput |
6,500 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
Soloviev D-136
|
| gptkbp:type |
turboshaft
|
| gptkbp:usedInAircraft |
gptkb:Mil_Mi-10
gptkb:Mil_Mi-6 gptkb:Mil_Mi-26 |
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Mil_Mi-12
|
| gptkbp:bfsLayer |
7
|