PSV stands for Perspektivny Skorostnoy Vertolyot) or “Advanced High-Speed Helicopter”

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: In development

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 (all retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Klimov VK-2500-01 turbine

Engine manufacturer: JSC Klimov United Engine Corporation

Max continuous power: 1417 kW (1900 hp)

Take-off / rated power: 1790 kW (2400 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 10590 kg (23347 lb)

Related VFS Resources

Resources related to the Mi-24LL PSV , provided by the Vertical Flight Society.
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Related Public Resources

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

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