Mil Mi-3

Additional modification of the Mil Mi-1, the Mi-3  is equipped with the AI-26V radial engine (same as the Mi-1T derivative).  The capacity is increased to a pilot and three passengers.  Main rotor blade count is increased to four; maximum payload is 230 kg.

The designation 'Mi-3' is reused for a modification of the later Mil Mi-2.

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 devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1 in Single seater arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

Mil Moscow Helicopter Plant 50 Years
Lyubimaya Kniga
1998 (page 46)
Book

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