Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:helicopter
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:crew |
1-2
|
| gptkbp:engine |
gptkb:Turbomeca_Arrius_2G1
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:feature |
modular design
coaxial rotors |
| gptkbp:firstFlight |
1997
|
| gptkbp:mainRotorDiameter |
13 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:maximumSpeed |
250 km/h
|
| gptkbp:maxTakeoffWeight |
3,600 kg
|
| gptkbp:operator |
gptkb:Russian_Air_Force
gptkb:Indian_Air_Force gptkb:Russian_Ministry_of_Emergency_Situations |
| gptkbp:range |
600 km
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:seatingCapacity |
up to 7
|
| gptkbp:serviceCeiling |
7,000 m
|
| gptkbp:variant |
gptkb:Kamov_Ka-226
|
| gptkbp:bfsParent |
gptkb:Ka-226
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Ka-226T
|