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Mil Mi-10The Mil Mi-10 (NATO reporting name Harke) was a Soviet military transport helicopter of flying crane configuration, developed from the Mi-6. Alsow known as "Product 60" by Rostov-upon-Don helicopter facility. It was built in long-legged and short-legged ("K") versions. Two 5500 shp Soloviev D-25 turboshafts. Development of 1962. Entered service in 1963. Variants - Mi-10K - crane
- Mi-10R - record setting
- Mi-10PP - ECM (Postanovschik Pomekh)
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)
- Main rotor diameter: 35.00 m (114 ft 10 in)
- Height: 7.80 m (25 ft 7 in)
- Main rotor area: 962 m² (10,350 ft²)
- Empty: 24,680 kg (54,296 lb)
- Loaded: 43,550 kg (95,810 lb)
- Maximum takeoff: 43,700 kg (96,140 lb)
- Powerplant: 2x Soloviev D-25V turboshafts, 4,045 kW (5,422 shp) each
Performance - Maximum speed: 204 km/h (128 mph)
- Range: 650 km (406 miles)
- Service ceiling: 3,000 m (9,840 ft)
- Rate of climb: m/min ( ft/min)
- Main rotor loading: 45 kg/m² (9 lb/ft²)
- Power/Mass: 0.18 kW/kg (0.11 hp/lb)
External links - http://www.aviation.ru/Mi/#10
Related content Related development: Mil Mi-6 Comparable aircraft: Designation sequence: Mi-6 - Mi-8 - Mi-9 - Mi-10 - Mi-12 - Mi-14 - Mi-17
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