Variant of the Mil Mi-24.  The helicopter was presented in Le Bourget at the Moscow Air Show '95; the design includes alternate controls for the gunner in the event the pilot is wounded.  Maximum internal and external payload are 1500 kg and 2400 kg, respectively.  Ammunition loading is 2860 kg.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Tandem

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Motor Sich TV3-117VMA turbine

Engine manufacturer: Motor Sich

Take-off / rated power: 1640 kW (2198 hp)

Intermediate power: 1618 kW (2169 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 11500 kg (25353 lb)

Max Range: 415 km (224 nm)

Related VFS Resources

Resources related to the Mi-24VM , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the Mi-24VM , provided by public sources across the internet.

Images