Mil Mi-10

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The Mil Mi-10 (NATO reporting name Harke) was a Soviet military transport helicopter of flying crane configuration, developed in 1962 from the Mi-6. It entered service in 1963.

Also known as "Product 60" by Rostov-upon-Don helicopter facility.

It was built as the short-legged ("Mi-10K") version, and the long-legged ("Mi-10R") version. It is powered by two 5500 shp Soloviev D-25 turboshafts.

[edit] Variants

• V-10 - Prototype of the Mil Mi-10 helicopter.
• Mi-10K - Short-legged flying crane helicopter (see pict. in flight in bulg. WIKI).
• Mi-10R - Standard production model, long-legged flying-crane helicopter. Record setting.
• Mi-10PP - ECM (Postanovschik Pomekh)

[edit] Operators

[edit] Military Operators

•  Soviet Union

[edit] Civil Operators

•  Soviet Union: Aeroflot

[edit] Specifications (Mil-10)

General characteristics

• Crew: Three
• Capacity: Up to 15,000 kg (33,000 lb) of cargo
• Length: 32.86 m (107 ft 9 in)
• Rotor diameter: 35.00 m (114 ft 10 in)
• Height: 7.80 m (25 ft 7 in)
• Disc area: 962 m² (10,350 ft²)
• Empty weight: 24,680 kg (54,296 lb)
• Loaded weight: 43,550 kg (95,810 lb)
• Max takeoff weight: 43,700 kg (96,140 lb)
• Powerplant: 2× Soloviev D-25V turboshafts, 4,045 kW (5,422 shp) each

Performance

• Maximum speed: 204 km/h (128 mph)
• Range: 650 km (406 mi)
• Service ceiling: 3,000 m (9,840 ft)
• Rate of climb: m/s (ft/min)
• Disc loading: 45 kg/m² (9 lb/ft²)
• Power/mass: 0.18 kW/kg (0.11 hp/lb)

[edit] External links

• http://www.aviation.ru/Mi/#10

[edit] Related content

Related development

Mil Mi-6

 

Designation sequence

Mi-6 - Mi-8 - Mi-9 - Mi-10 - Mi-12 - Mi-14 - Mi-17

 

 

The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.