Mil Mi-10

Attribution

Attribution

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

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-10

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

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

Data on aircraft size

Overall Height: 9.80 m (32.2 ft)

Overall Length: 41.89 m (137.4 ft)

Overall Width: 35.00 m (114.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Soloviev D-25V turbine

Engine manufacturer: Soloviev Design Bureau

Take-off / rated power: 4103 kW (5500 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 43450 kg (95790 lb)

Max Range: 430 km (232 nm)

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