Development of the Mi-24 (NATO Designation: 'Hind'), a Russian transport attack helicopter, began in 1967.  In the design, the cockpit is divided per pilot with separately pressurized cabins.  Either TV3-117 (2200 shp) or TV3-117V (2225 shp) turbine engines may be used for the twin-engine aircraft.  Approved on 19 February, 1969; official testing started in June of 1970.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 2-3 in Tandem arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

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Related Public Resources

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