The Ka-62 is a multipurpose helicopter with maximum internal and slung payloads of 2000 and 2500 kg, respectively.  The cabin can carry up to 16 passengers in addition to the pilots.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 13.80 m (45.3 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Ardiden 3G turbine

Engine manufacturer: Turbomeca

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 6500 kg (14330 lb)

Max Range: 770 km (416 nm)

Max Endurance: 4.0 hrs (4.0 hrs)

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