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Mi-26

Mi-26

Utility & Transport Helicopters
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Basic Information
Name
Mi-26
Designation
Mi-26
Alternate Designation
Equipment Type
Utility & Transport Helicopters
Manufacturer
Date of Introduction
Description

The Mil Mi-26, Halo NATO-codename, is a day/night, all-weather, heavyweight helicopter designed to transport troops, vehicles, and cargo as well as to perform medical evacuation missions. Additional airlift capability is provided using an external sling. The Mi-26 is the world's largest helicopter with an impressive 20,000 kg payload capacity and 14 unmatched world records. The Mi-26 follows traditional helicopter scheme with an eight-blade main rotor and five-blade tail rotor. It is powered by two D-136 engines providing 10,000-hp each with reduced fuel consumption. The crew cabin has been hardened to withstand small arms impact, redundant sub-systems and special protection for hot-parts as well as other measures ensure enhanced survivability for the valuable Mi-26 helicopter. It can be fitted with engine exhaust heat suppressers and chaff/flare dispensers to improve survivability. The Mi-26 rear compartment can accommodate one armored vehicle through a loading ramp provided to facilitate loading and unloading operations. Up to 82 fully equipped troops can be transported inside a single Mi-26 helicopter and the medical evacuation configuration (Mi-26MS) allows to accommodate 60 casualties with medical equipment and one operation room. The Mi-26 Halo cargo helicopter, also known as Mi-26T, was introduced in the Soviet Army in 1983 replacing Mi-6 Hook helicopters. The Mi-26TS is a variant designed for the civilian market. Mi-26TZ is tanker helicopter and Mi-26M is an improved version intended for replacement of remaining Mi-6 helicopters in the Russian Army. According to Mil around 280 Mi-26 helicopters were produced from 1982 through 1999.

Overview (Deagel)
Group Utility & Transport Helicopters
Status Active
Also Known As Halo, Hoodlum, Mi-26M, Mi-26MS, Mi-26T, Mi-26TS (Mi-26TC? firefighting helicopter), Mi-26TZ
Origin Russia
Contractor Mil Helicopter
Initial Operational Capability (IOC) 1983
Total Production 311
Specifications (Deagel)
Crew 5
Main Rotor Blades 8
Number of Engines 2
Troops 82
Dimensions — Height 8.2 meter
Dimensions — Length 33.8 meter
Dimensions — Main Rotor Diameter 32 meter
Dimensions — Width 6.2 meter
Mass — Max Takeoff Weight 56,000 kilogram
Mass — Payload 20,000 kilogram
Performance — Ceiling 4,600 meter
Performance — Max Range 800 kilometer
Performance — Min Range 590 kilometer
Power — Max Power at TakeOff 20,000 shp
Speed — Cruise Speed 71 mps
Speed — Top Speed at High Altitude 82 mps
Gear (Deagel)
Item 1 Jamming Systems: President-S (1)
Item 2 Turboshaft Engines: D-136 (2)
Variants
Variant 1 Mi-26
Variant 2 Mi-26T2
Variant 3 Mi-26T2VA
Details
Country of Origin Russia
Category Transport Helicopter
Air > Transport Helicopter
Classification
Domain
Air & Air Defense
Equipment Status
Active
Related Equipment (1)
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