The first prototype of the Mil Mi-2.  Developed with the intention of a multipurpose helicopter.  The listed Max takeoff weight of 3197 kg is from the Agricultural version.  Production began in 1961.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: No type defined

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: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 14.50 m (47.6 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Klimov GTD-350 turbine

Engine manufacturer: JSC Klimov United Engine Corporation

Take-off / rated power: 298 kW (400 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 3197 kg (7048 lb)

Max Range: 300 km (162 nm)

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