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gptkbp:instance_of
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gptkb:helicopter
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Ka-226
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|
gptkbp:armament
|
optional machine guns
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|
gptkbp:avionics
|
modern digital systems
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|
gptkbp:combat_role
|
transport and reconnaissance
|
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gptkbp:crew
|
2
1-2
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|
gptkbp:design
|
twin-engine
|
|
gptkbp:diameter
|
14.5 m
two-blade
fenestron
|
|
gptkbp:ecological_role
|
operates in harsh conditions
|
|
gptkbp:engine
|
450 hp
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:exported_to
|
several countries
|
|
gptkbp:features
|
high maneuverability
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:fuel_capacity
|
800 L
|
|
gptkbp:future_plans
|
upgraded versions in development
|
|
gptkbp:height
|
3.6 m
|
|
gptkbp:historical_event
|
developed from Ka-26
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ka-226 S
|
|
gptkbp:is_used_by
|
gptkb:Indian_Armed_Forces
|
|
gptkbp:landing_gear
|
skids
|
|
gptkbp:length
|
8.6 m
|
|
gptkbp:maintenance
|
easy to maintain
|
|
gptkbp:manufacturer
|
gptkb:Kamov
|
|
gptkbp:market_segment
|
commercial and military
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
3200 kg
|
|
gptkbp:military_technology
|
gptkb:railway_line
|
|
gptkbp:modifications
|
search and rescue variant
|
|
gptkbp:notable_features
|
modular design
|
|
gptkbp:number_built
|
over 100
|
|
gptkbp:operational_history
|
used in various missions
|
|
gptkbp:operational_range
|
500 km
|
|
gptkbp:origin
|
gptkb:Russia
|
|
gptkbp:performance
|
excellent hover performance
|
|
gptkbp:primary_user
|
Russia, India
|
|
gptkbp:produced_by
|
in production
|
|
gptkbp:production_years
|
gptkb:2002
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_features
|
crashworthy design
|
|
gptkbp:seating_capacity
|
gptkb:6
1500 kg
1000 kg
|
|
gptkbp:service_ceiling
|
5000 m
|
|
gptkbp:training
|
pilot training
|
|
gptkbp:type
|
light helicopter
|
|
gptkbp:variant
|
gptkb:Ka-226_T
|