Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:configuration |
axial-centrifugal compressor
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.45 m
|
| gptkbp:family |
TV3-117
|
| gptkbp:firstFlight |
1974
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
TV3-117VMA
|
| gptkbp:length |
1.98 m
|
| gptkbp:manufacturer |
gptkb:Klimov
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:powerOutput |
2200 hp
|
| gptkbp:usedInAircraft |
gptkb:Kamov_Ka-32
gptkb:Mil_Mi-8 gptkb:Kamov_Ka-29 gptkb:Mil_Mi-17 gptkb:Kamov_Ka-50 gptkb:Kamov_Ka-52 gptkb:Kamov_Ka-27 |
| gptkbp:weight |
330 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_TV3-117
gptkb:TV3-117_engine |
| gptkbp:bfsLayer |
7
|