Mi-26 K

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:helicopter
gptkbp:bfsLayer 5
gptkbp:bfsParent gptkb:Mil_Mi-26
gptkb:Mi-26
gptkbp:armament gptkb:none
gptkbp:avionics modernized
gptkbp:climb_rate 5 m/s
gptkbp:country several countries
gptkbp:crew gptkb:5
gptkbp:design cargo transport
gptkbp:diameter fenestron
32.0 m
gptkbp:engine 11,400 shp
gptkbp:engine_type turboshaft
gptkbp:first_flight gptkb:1980
gptkbp:fuel_capacity 3,000 L
gptkbp:height 8.1 m
gptkbp:historical_event developed from Mi-26
https://www.w3.org/2000/01/rdf-schema#label Mi-26 K
gptkbp:landing_gear retractable
gptkbp:length 40.0 m
gptkbp:manufacturer gptkb:Mil_Moscow_Helicopter_Plant
gptkbp:material aluminum alloy
gptkbp:max_speed 295 km/h
gptkbp:max_takeoff_weight 56,000 kg
120 m³
gptkbp:military_technology gptkb:Mi-26_T
gptkbp:modifications various configurations available
gptkbp:nickname gptkb:Halo
gptkbp:notable_features heavy lift capability
gptkbp:number_built over 300
gptkbp:operational_history used in various conflicts
gptkbp:operational_range 1,000 km
gptkbp:operational_status active
gptkbp:origin gptkb:Russia
gptkbp:primary_user gptkb:Russian_Armed_Forces
gptkbp:production_years gptkb:1980
present
gptkbp:propulsion twin-engine
gptkbp:range 800 km
gptkbp:role transport helicopter
heavy transport
gptkbp:safety_features advanced avionics
gptkbp:seating_capacity gptkb:television_series
gptkb:battle
up to 20 tons
20,000 kg
side door
gptkbp:service_ceiling 4,600 m
gptkbp:services gptkb:1983
gptkbp:type gptkb:helicopter
gptkbp:variant gptkb:Mi-26
gptkbp:wingspan 32.0 m