Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:configuration |
axial-centrifugal compressor
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.38 m
|
| gptkbp:family |
TV3-117
|
| gptkbp:firstFlight |
1974
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
TV3-117MT
|
| gptkbp:length |
2.09 m
|
| gptkbp:manufacturer |
gptkb:Klimov
gptkb:Motor_Sich |
| gptkbp:numberOfAxles |
2
|
| gptkbp:numberOfStages |
2
10 |
| gptkbp:powerOutput |
1900 shp
|
| gptkbp:usedIn |
gptkb:Mil_Mi-17
gptkb:Mil_Mi-24 gptkb:Mil_Mi-35 Mil Mi-8MT |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_TV3-117
gptkb:TV3-117_engine |
| gptkbp:bfsLayer |
7
|