Mil Mi-10
From Wikipedia, the free encyclopedia
| Mi-10 | |
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Mil Mi-10 (Harke) at Monino Central Air Force Museum (Moscow) |
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| Type | Skycrane |
| National origin | Russia |
| Manufacturer | Mil |
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. The Mi-10 uses a closed circuit camera system that scans forward from under the rear fuselage and downward through the sling hatch to watch the payload and landing gear and for touchdown. [1]
[edit] Variants
- V-10 - Prototype of the Mil Mi-10 helicopter.
- Mi-10K (NATO - Harke-B) - Short-legged flying crane helicopter, with a narrower-tracked undercarriage, and equipped with a ventral gondola. (see [[1]]).
- Mi-10R (NATO - Hark-A) - Standard production model, long-legged flying-crane helicopter. Record setting.
- Mi-10PP - ECM (Postanovschik Pomekh)
[edit] Operators
[edit] Military Operators
[edit] Civil Operators
- UTair (7)
[edit] Former operators
[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] See also
Related development
Comparable aircraft
[edit] References
[edit] External links
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The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.

