Light single-seat coaxial helicopter developed by the Kamov Design Bureau in 1949; there is no fuselage.  NATO Designation of the Kamov Ka-10 is Hat.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-10

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: Floats

Overall Dimensions

Data on aircraft size

Overall Height: 2.50 m (8.2 ft)

Overall Length: 5.80 m (19.0 ft)

Overall Width: 5.80 m (19.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Ivchenko AI-4G reciprocating

Engine manufacturer: Ivchenko

Take-off / rated power: 40 kW (54 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 370 kg (816 lb)

Max Range: 170 km (92 nm)

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