Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
1 or 2
|
| gptkbp:developedBy |
gptkb:Kamov_Ka-26
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:exportedTo |
gptkb:India
|
| gptkbp:firstFlight |
1997
|
| gptkbp:height |
4.15 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kamov Ka-226 helicopter
|
| gptkbp:length |
8.1 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
3,600 kg
|
| gptkbp:notableFeature |
modular mission pod
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:range |
600 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:seatingCapacity |
up to 7
|
| gptkbp:serviceCeiling |
6,000 m
|
| gptkbp:status |
in service
|
| gptkbp:tailRotorType |
coaxial rotors
|
| gptkbp:usedBy |
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force gptkb:Russian_Ministry_of_Emergency_Situations |
| gptkbp:variant |
gptkb:Ka-226AG
gptkb:Ka-226T |
| gptkbp:bfsParent |
gptkb:SPT_240
gptkb:VA-63E |
| gptkbp:bfsLayer |
8
|