Introduction:
The Mil Mi-26 is the world’s heaviest-lift helicopter in serial production, able to carry up to 20 tons of cargo in its cabin or on an external sling. The first prototype flew in 1977 with pre-production machines were from 1980, production machines sometime after that.

The Mi-26T model used as a basic civillian freighter has a BREO-28 Airborne Electronic System which provides up to date real time information to the piolots allowing them to fly in adverse weather conditions.
Other versions are the Mi-26A with automated approach and descent avionics, Mi-26MS medevac version, Mi-26P 63 passenger airliner, Mi-26TM flying crane with under nose gondola to allow supervision of sling operations, and Mi-26TZ fuel tanker and the new Mi-26M which features a new 1a 0,700kW class ZMKB Progress D127 turboshafts, better hot and high performance, increased maximum payload, composite main rotor blades, improved aerodynamics and EFIS flightdeck.
General Characteristics:
Crew: Five– 2 pilots, 1 navigator, 1 flight engineer, 1 flight technician
Capacity: 90 passangers, 20,000 kg cargo
Length: 40.025 m (rotors turning)
Rotor diameter: 32.00 m
Height: 8.145 m
Disc area: 804.25 m2
Empty Weight: 28,200 kg
Loaded weight: 49,600 kg
Max. takeoff weight: 56,000 kg
Powerplant: 2 × Lotarev D-136 turboshafts 8,500 kW each
Performance:
Max. speed: 295 km/hr
Cruise Speed: 255 km/hr
Range: 1,920 km (with auxiliary tanks)
Service Ceiling: 4,600m
Operating Temperature Range: Down to -60 Deg C
Central Asia:

No comments:
Post a Comment