Modification of the Mil Mi-1.  Can be fitted with external tanks. Maximum sling load is 500 kg.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-1

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: 14.30 m (46.9 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Ivchenko AI-26VF reciprocating

Engine manufacturer: Ivchenko

Take-off / rated power: 459 kW (615 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2550 kg (5622 lb)

Max Range: 360 km (194 nm)

Related VFS Resources

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Related Public Resources

Resources related to the Mi-1M , provided by public sources across the internet.

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