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Military


Mi-10 Harke

Specifications
Country of Origin Russia
Builder Mil
Role Heavy transport (65 equipped troops), vehicles
Variants
  • V-10 - Prototype of the Mil Mi-10 helicopter.
  • Mi-10K - Short-legged flying crane helicopter.
  • Mi-10R - Standard production model, long-legged flying-crane helicopter. Record setting.
  • Mi-10PP - ECM (Postanovschik Pomekh)
  • Length 32.86 m (107 ft 9 in)
    length with rotors turning 41.89 meters (137 feet 5.25 inches)
    Rotor diameter 35.00 m (114 ft 10 in)
    Height 7.80 m (25 ft 7 in)
    Empty weight 24,680 kg (54,300 lb)
    Loaded weight 43,550 kg (95,810 lb)
    maximum take-off with the load on the suspension 38000 kg (83,776 pounds)
    Max takeoff weight 43,700 kg (96,140 lb)
    Capacity Up to 15,000 kg (33,000 lb) of cargo
    Powerplant 2 Soloviev D-25V turboshafts, 4101 kW (5500 hp) each
    Maximum speed 204 km/h (128 mph)
    maximum cruising speed of the load on the suspension 202 kilometers per hour (125 miles / hour)
    Range 650 km (410 miles)
    range with standard payload 250 kilometers (155 miles)
    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)
    Crew Three
    Type Mi-10 Mi-10K
    Year of manufacture 1960 1966
    Crew 3 3 to 4
    Passengers - -
    Powerplant D-25V D-25V
    Take-off power, hp 2 5,500 2 5,500
    Main rotor diameter, m 35 35
    Empty weight, kg 27,100 25,450
    Take-off weight, kg
          normal 43,550 37,000
          maximum 43,700 38,000
    Payload, kg:
          normal 12,000 3,000*
          maximum 15,000 -
          external 8,000 11,000
    Speed, km/h:
          maximum 204 256
          cruising 180 228
    Hovering ceilingout of ground effect, m: - 1,000
    Hovering ceiling in ground effect, m: - 3,000
    Service ceiling, m 3,000 4,750
    Operational range, km 430 500

    * Inside the cargo cabin




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