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Mi-26 is a multi-purpose wide-fuselage transport helicopter. It is intended for freight of vehicles, both self-propelled and non-self-propelled, and large-size cargoes up to 20 tons either inside the cargo compartment or on the external sling.
A combined internal and external load up to 20 tons maximum is also possible.
MI-26 CAN BE SUCCESSFULLY APPLIED IN:
- an assault version for transportation of 82 paratroopers;
- an ambulance version for accomodation of 60 casualties on stretchers accompanied by 3 medical assistants;
- a converted (module) medical complex version for reanimation and evacuation of casualties;
- a refueler version for delivery and distribution to the consumers of fuel (kerosene and disel fuel) and lubricants.
The cargo compartment is equipped with a 6 ton hoisting device and two electric winches. A clearance control system is available for handling large-size cargo.
The helicopter is provided with means of passive interferences, and radar illumination warnng equipment.
The helicopter is equipped with avionics allowing its operation on international routes, day or night flying in extreme weather conditions.
The cockpit is very comfortable, armored, pressurized, has an air conditioning system, excellent visibility.
Design and equipment of the helicopter allow its autonomous operation where ground facilities are not available.
PERFORMANCE
Engine D-136 ..................................... 2x11.400 hp
Take-off weight:
normal.................................................. 49.6 t
maximum ............................................. 56.O t
empty weight........................................ 28.6 t
Load-carrying capacity:
in cargo compartment and
on an external sling ............................... 20.0 t
dimensions of cargo cabin 12.1 x3.29x3.17 m
cruising speed per hour..................... 255 km
Ceiling under ISA conditions (at normal take-off weight):
hovering OGE (minimum)................. 1.520 m
service (minimum)........................... 4.600 m
Range:
standard tanks................................... 800 km
four extra tanks .............................. 1.920 km
Diameter of main rotor............................... 32.0 m
Number of blades................................................ 8
Crew................................................................... 5
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