Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
1 or 2
|
| gptkbp:designedFor |
high-altitude operations
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
2016
|
| gptkbp:height |
4.15 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ka-226AG
|
| gptkbp:jointProduction |
gptkb:Hindustan_Aeronautics_Limited
|
| gptkbp:length |
8.1 m
|
| gptkbp:mainRotorDiameter |
13 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
3,600 kg
|
| gptkbp:notableFeature |
modular design
no tail rotor |
| gptkbp:powerplant |
Safran Arrius 2G1 engines
|
| gptkbp:primaryUser |
gptkb:Indian_Armed_Forces
|
| gptkbp:range |
600 km
|
| gptkbp:regionOfOrigin |
gptkb:India
gptkb:Russia |
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:rotorConfiguration |
coaxial rotors
|
| gptkbp:seatingCapacity |
up to 7
|
| gptkbp:variant |
gptkb:Kamov_Ka-226
|
| gptkbp:bfsParent |
gptkb:Ka-226_helicopter
gptkb:Ka-226 |
| gptkbp:bfsLayer |
6
|