|
gptkbp:instance_of
|
gptkb:helicopter
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:CH-53_Sea_Stallion
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modernized avionics
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Mikhail_Mil
|
|
gptkbp:diameter
|
gptkb:4
gptkb:6
32.0 m
|
|
gptkbp:emergency_services
|
dual hydraulic systems
|
|
gptkbp:engine_type
|
turbo-shaft
|
|
gptkbp:first_flight
|
gptkb:1977
|
|
gptkbp:fuel_capacity
|
13,000 L
|
|
gptkbp:height
|
8.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mi-26 Halo
|
|
gptkbp:introduced
|
gptkb:1983
|
|
gptkbp:length
|
40.0 m
|
|
gptkbp:manufacturer
|
gptkb:Mil_Moscow_Helicopter_Plant
|
|
gptkbp:max_speed
|
295 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
1,200 m
56,000 kg
|
|
gptkbp:military_technology
|
gptkb:Mi-26
gptkb:Mi-26_T
|
|
gptkbp:notable_users
|
gptkb:India
gptkb:Kazakhstan
gptkb:Russia
gptkb:Ukraine
gptkb:Azerbaijan
|
|
gptkbp:operational_area
|
gptkb:mythological_figure
disaster relief
medical evacuation
heavy lift
aerial firefighting
construction support
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:power_output
|
11,400 hp
|
|
gptkbp:produced_by
|
over 300
|
|
gptkbp:production_years
|
gptkb:1980
gptkb:2002
|
|
gptkbp:range
|
800 km
|
|
gptkbp:role
|
transport helicopter
|
|
gptkbp:safety_features
|
crashworthy seats
|
|
gptkbp:seating_capacity
|
90
20,000 kg
3.2 m x 3.2 m x 12.5 m
|
|
gptkbp:service_ceiling
|
4,500 m
|
|
gptkbp:variant
|
gptkb:Mi-26_T
|
|
gptkbp:wingspan
|
32.0 m
|