Mil Mi-10
The Mil Mi-10, designated Harke by NATO, is a heavy cargo transport helicopter. It stands with four legs, and holds loads beneath the fuselage secured with hydraulic locks. Maximum payload is 15000 kg--on a sling, the maximum payload is 8000 kg.
Source: Milling into Western Markets, FLIGHT International 23 March 1967
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 2
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Layout and Dimensions
Data on aircraft size| Overall Dimensions | ||
|---|---|---|
| Overall Height: | 9.80 m | 32.2 ft |
| Overall Length: | 41.89 m | 137.4 ft |
| Overall Width: | 35.00 m | 114.8 ft |
| Airframe Dimensions | ||
|---|---|---|
| Airframe Length: | 32.86 m | 107.8 ft |
| Airframe Width: | ||
| Airframe Height: | ||
| Landing Gear Dimensions | ||
|---|---|---|
| Landing Gear Base: | 8.29 m | 27.2 ft |
| Landing Gear Track: | ||
| Cabin Dimensions | ||
|---|---|---|
| Cabin Internal Height: | ||
| Cabin Internal Length: | ||
| Cabin Internal Width: | ||
Weights and Performance
Data on aircraft weight and flight characteristics| Weights | ||
|---|---|---|
| Max Gross Weight (ground): | 43,450 kg | 95,790 lb |
| Max Gross Weight (airborne): | ||
| Max Take-off Weight: | 43,450 kg | 95,790 lb |
| Empty Weight: | 27,100 kg | 59,745 lb |
| Useful Load: | 16,350 kg | 36,045 lb |
| Empty Weight Fraction: | 0.624 | |
| Climb Performance | ||
|---|---|---|
| Max Rate of Climb: | ||
| Hover Performance | ||
|---|---|---|
| Hover Ceiling IGE: | ||
| Hover Ceiling OGE: | ||
| Limitations | ||
|---|---|---|
| Max Level Flight Speed: | 204 km/h | 110 kts |
| Never Exceed Speed: | ||
| Service Ceiling: | 3,000 m | 9,843 ft |
| Range and Endurance | ||
|---|---|---|
| Max Range: | 430 km | 232 nm |
| Max Endurance: | ||
Engine Details
Aircraft powerplant (lift and/or propulsion)Provided powerplant data is for uninstalled, sea level, static operations.
| Powerplant | ||
|---|---|---|
| Number of engines: | 2 | |
| Designation: | Soloviev D-25V turbine | |
| Manufacturer: | Soloviev Design Bureau | |
| Normal Ratings | ||
|---|---|---|
| Max continuous: | ||
| Take-off / rated: | 4103 kW | 5500 hp |
| Intermediate: | ||
| Maximum: | ||
| OEI Ratings | ||
|---|---|---|
| OEI contingency: | ||
| OEI continuous: | ||
| OEI 30-second: | ||
| OEI intermediate: | ||
Primary Lift Device
Data on primary lift devices such as main rotors| Main Rotor Characteristics | ||
|---|---|---|
| Diameter: | 35.00 m | 114.83 ft |
| RPM: | 220.0 rpm | 220.0 rpm |
| Direction of Rotation: | Clockwise | |
| Hub Type: | ||
| Main Rotor Blade Characteristics | ||
|---|---|---|
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Tip Geometry: | Conventional | |
| Blade Twist: | ||
| Number of Blades: | 5 | |
| Main Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | 962.11 m² | 10356.5 ft² |
| Disc Loading: | 45.16 kg/m² | 9.250 lb/ft² |
| Solidity: | ||
| Main Rotor Blade Derived Characteristics | ||
|---|---|---|
| Blade area per blade: | ||
| Tip Speed: | 403.17 m/s | 1322.7 fps |
Primary Control Device
Data on primary control devices such as tail rotors| Tail Rotor Characteristics | ||
|---|---|---|
| Diameter: | 6.30 m | 20.67 ft |
| Configuration: | Pusher | |
| Direction of Rotation: | Top blade fwd | |
| RPM: | ||
| Tail Rotor Blade Characteristics | ||
|---|---|---|
| Number of Blades: | 4 | |
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Twist: | ||
| Tail Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | 31.17 m² | 335.5 ft² |
| Solidity: | ||
| Tail Rotor Blade Derived Characteristics | ||
|---|---|---|
| Tip Speed: | ||
| Blade Area (per blade): | ||
Related VFS Resources
Resources related to the Mi-10 , provided by the Vertical Flight Society.Forum Proceedings
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