Mil Mi-10
Air-Crane Helicopter
The Mil Mi-10 is a twin-engined heavy transport-helicopter and crane-helicopter developed by the Soviet manufacturer Mil OKB, today MIL Moscow helicopter plant, JSC (Russia).
The Mil Mi-10 is a development of the
Mil Mi-6. Two different variants were produced, the Mi-10R with high landing gear and the Mi-10K with low landing gear. The maximum external load is approx. 11 tons (24250 lbs).
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Soloviev D-25V(W) |
| Engine Power (each) | 4045 kW | 5424 shp |
| Speed | 202 km/h | 109 kts
125 mph |
| Service Ceiling | 3.000 m | 9.842 ft |
| Range | 250 km | 135 NM
155 mi. |
| Empty Weight | 24.680 kg | 54.410 lbs |
| max. Takeoff Weight | 38.000 kg | 83.776 lbs |
| Rotor Blades (main/tail) | 5/4 |
| Main Rotor Diameter | 35,00 m | 114 ft 10 in |
| Tail Rotor Diameter | 6,30 m | 20 ft 8 in |
| Rotor Disc Area | 962,1 m² | 10356 ft² |
| Length (Fuselage) | 32,90 m | 107 ft 11 in |
| Length | 41,89 m | 137 ft 5 in |
| Height | 7,80 m | 25 ft 7 in |
| First Flight | 1960 |
| Production Status | out of production |
| Total Production | 55 |
| Developed from | Mil Mi-6 |
| ICAO Code | MI10 |
| NATO Code | Harke |
| Data for (Version) | Mil Mi-10K |
| Variants | Mi-10R, Mi-10K |
