A modification of the Ka-10, the Ka-15 has a closed fuselage.  The aircraft may be equipped with floats for landing gear.  NATO Designation of the helicopter is Hen.  The cabin can seat a single passenger in additon to the pilot.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-15

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Coaxial (x2)

Crew required: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 3.35 m (11.0 ft)

Overall Length: 9.96 m (32.7 ft)

Overall Width: 9.96 m (32.7 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Ivchenko AI-14V reciprocating

Engine manufacturer: Ivchenko

Take-off / rated power: 188 kW (252 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1370 kg (3020 lb)

Max Range: 350 km (189 nm)

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