The first Russian naval helicopter, designated Hormone by NATO.  Its first prototype took flight in 1961.  Its coaxial rotors can be folded for storage and transport.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-25

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Coaxial (x2)

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Wheels (some retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.37 m (17.6 ft)

Overall Width: 15.74 m (51.6 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Glushenkov GTD-3BM turbine

Engine manufacturer: Glushenkov

Take-off / rated power: 738 kW (989 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 7500 kg (16535 lb)

Max Range: 400 km (216 nm)

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