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gptkbp:instance_of
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gptkb:helicopter
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cargo_capacity
|
1,500 kg
1,000 kg
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:crew
|
2
|
|
gptkbp:cruise_speed
|
220 km/h
|
|
gptkbp:design_feature
|
modular design
high maneuverability
short takeoff and landing capability
coaxial rotors
|
|
gptkbp:diameter
|
14.5 m
|
|
gptkbp:engine_type
|
turboshaft
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:height
|
4.6 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ka-226 helicopter
|
|
gptkbp:length
|
15.9 m
|
|
gptkbp:manufacturer
|
gptkb:Kamov
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
3,200 kg
|
|
gptkbp:notable_case
|
none reported
|
|
gptkbp:notable_users
|
gptkb:Brazil
gptkb:India
gptkb:Kazakhstan
gptkb:Mexico
gptkb:Russia
|
|
gptkbp:operational_range
|
600 km
|
|
gptkbp:operational_use
|
gptkb:transportation
gptkb:search_and_rescue
medical evacuation
agricultural applications
firefighting
|
|
gptkbp:passenger_capacity
|
gptkb:6
|
|
gptkbp:power_source
|
TV3-117
|
|
gptkbp:produces
|
over 200
|
|
gptkbp:production_years
|
gptkb:1997
present
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
gptkb:helicopter
|
|
gptkbp:safety_features
|
redundant systems
crashworthy design
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:variant
|
gptkb:Ka-226_S
gptkb:Ka-226_T
|
|
gptkbp:weight
|
1,800 kg
|
|
gptkbp:bfsParent
|
gptkb:Russian_Helicopters_Holding_Company
|
|
gptkbp:bfsLayer
|
8
|