The Mi-28A is an antitank helicopter, a variant of the Mil Mi-28.  It is quipped with a 30 mm gun moun, armor, and shock abosorbant seats and landing gear.  The TV3-117VMA turboshaft engines have deflectors and separators for the prevention of dust ingestion.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-28

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

Overall Height: 4.81 m (15.8 ft)

Overall Length: 16.85 m (55.3 ft)

Overall Width: 17.20 m (56.4 ft)

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: 460 km (248 nm)

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