Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Ka-226
|
| gptkbp:armament |
optional machine guns
|
| gptkbp:avionics |
modern avionics suite
|
| gptkbp:crew |
2
|
| gptkbp:design |
twin-engine
|
| gptkbp:diameter |
14.5 m
|
| gptkbp:engine |
T V3-117
|
| gptkbp:first_flight |
gptkb:2002
|
| gptkbp:height |
3.6 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ka-226 M
|
| gptkbp:is_used_by |
gptkb:Indian_Armed_Forces
|
| gptkbp:length |
8.6 m
|
| gptkbp:manufacturer |
gptkb:Kamov
|
| gptkbp:max_speed |
250 km/h
|
| gptkbp:max_takeoff_weight |
3,200 kg
|
| gptkbp:origin |
gptkb:Russia
|
| gptkbp:production_years |
gptkb:2002
|
| gptkbp:propulsion |
turboshaft engines
|
| gptkbp:range |
600 km
|
| gptkbp:role |
gptkb:public_transportation_system
gptkb:mythological_figure gptkb:helicopter medical evacuation firefighting agricultural operations |
| gptkbp:seating_capacity |
gptkb:6
1,000 kg |
| gptkbp:service_ceiling |
5,000 m
|
| gptkbp:variant |
gptkb:Ka-226_T
|