| 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
|
