Mil Mi-10
Photo ©: Olafur Sigurdsson (Photos at airliners.net)
Mi-10
Air-Crane Helicopter
| Crew | 3 | |
| Propulsion | 2 Turboshaft Engines | |
| Engine Model | Solowjew / Soloviev D-25V | |
| Engine Power (each) | 4048 kW | 5428 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 | 5/4 |
| Main Rotor Diameter | 35,00 m | 114,8 ft |
| Tail Rotor Diameter | 6,30 m | 20,7 ft |
| Rotor Disc Area | 962,1 m² | 10356 ft² |
| Length (Fuselage) | 32,90 m | 107,9 ft |
| Length | 41,89 m | 137,4 ft |
| Height | 7,80 m | 25,6 ft |
| First Flight | 1960 | |
| Production Status | out of production | |
| Total Production | 55 | |
| Developed from | Mil Mi-6 | |
| NATO Code | Harke | |
| Data for (Version) | Mil Mi-10K | |
Remarks
Based on Mil Mi-6.
| Weblinks | Extras |
| MIL Moscow helicopter plant, JSC |
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