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
VTOL 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)
Overall Dimensions | ||
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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 | ||
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Airframe Length: | 32.86 m | 107.8 ft |
Airframe Width: | ||
Airframe Height: |
Landing Gear Dimensions | ||
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Landing Gear Base: | 8.29 m | 27.2 ft |
Landing Gear Track: |
Cabin Dimensions | ||
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Cabin Internal Height: | ||
Cabin Internal Length: | ||
Cabin Internal Width: |
Weights | ||
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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 | ||
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Max Rate of Climb: |
Hover Performance | ||
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Hover Ceiling IGE: | ||
Hover Ceiling OGE: |
Limitations | ||
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Max Level Flight Speed: | 204 km/h | 110 kts |
Never Exceed Speed: | ||
Service Ceiling: | 3,000 m | 9,843 ft |
Range and Endurance | ||
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Max Range: | 430 km | 232 nm |
Max Endurance: |
Provided powerplant data is for uninstalled, sea level, static operations.
Powerplant | ||
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Number of engines: | 2 | |
Designation: | Soloviev D-25V turbine | |
Manufacturer: | Soloviev Design Bureau |
Normal Ratings | ||
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Max continuous: | ||
Take-off / rated: | 4103 kW | 5500 hp |
Intermediate: | ||
Maximum: |
OEI Ratings | ||
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OEI contingency: | ||
OEI continuous: | ||
OEI 30-second: | ||
OEI intermediate: |
Main Rotor Characteristics | ||
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Diameter: | 35.00 m | 114.83 ft |
RPM: | 220.0 rpm | 220.0 rpm |
Direction of Rotation: | Clockwise | |
Hub Type: |
Main Rotor Blade Characteristics | ||
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Blade Construction: | ||
Blade Chord: | ||
Blade Tip Geometry: | Conventional | |
Blade Twist: | ||
Number of Blades: | 5 |
Main Rotor Derived Characteristics | ||
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Disc Area: | 962.11 m² | 10356.5 ft² |
Disc Loading: | 45.16 kg/m² | 9.250 lb/ft² |
Solidity: |
Main Rotor Blade Derived Characteristics | ||
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Blade area per blade: | ||
Tip Speed: | 403.17 m/s | 1322.7 fps |
Tail Rotor Characteristics | ||
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Diameter: | 6.30 m | 20.67 ft |
Configuration: | Pusher | |
Direction of Rotation: | Top blade fwd | |
RPM: |
Tail Rotor Blade Characteristics | ||
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Number of Blades: | 4 | |
Blade Construction: | ||
Blade Chord: | ||
Blade Twist: |
Tail Rotor Derived Characteristics | ||
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Disc Area: | 31.17 m² | 335.5 ft² |
Solidity: |
Tail Rotor Blade Derived Characteristics | ||
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Tip Speed: | ||
Blade Area (per blade): |