Ka-60 Kasatka

🇷🇺Russian Federation
Kamov JSC
2010 – Present
Overview
Ka-60 Kasatka
The Ka-60 Kasatka is a medium weight transport helicopter developed by Kamov, featuring a twin-engine design and a four-blade main rotor.
Specifications

General

Crew2
Engines2
Range Km700 km
Max Speed Kmh291 km/h
Weight Max Kg6,500 kg
Cabin Capacity14
Cargo Sling Kg2,750 kg
Cargo Internal Kg2,000 kg
Service Ceiling M5,200 m
Main Rotor Diameter M13.5 m
Research Notes

Development history

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Ka-60 was Kamov's attempt to enter the medium utility helicopter class with a conventional tail-rotor layout.

The Ka-60 Kasatka was developed by Kamov as a medium utility and transport helicopter, unusual for the bureau because it adopted a single main rotor and tail rotor instead of Kamov's familiar coaxial arrangement. The program began as a potential military transport, reconnaissance, and special-mission aircraft but suffered long delays, engine issues, and limited prototype activity. Its civil derivative, the Ka-62, carried some of the design logic forward. The Ka-60 is therefore important as a design departure and as evidence of Russia's effort to modernize the light-medium helicopter segment.

Technical profile

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The design uses twin turboshafts, a medium cabin, and transport-oriented systems rather than heavy attack specialization.

Technically, Ka-60 was intended as a medium transport and utility helicopter capable of carrying troops, cargo, or mission equipment. Its configuration included twin turboshaft engines, a streamlined fuselage, wheeled landing gear, and a shrouded or compact tail-rotor arrangement in later related concepts. The aircraft was not designed as a dedicated attack helicopter, although military variants could support reconnaissance, command, or light mission packages. Its profile fills the space between small liaison helicopters and heavier Mi-8-class transports.

Operational use

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The Ka-60 remained limited, but its intended role shows Russia's need for a modern medium utility helicopter.

Operational use of Ka-60 itself appears limited because the program did not mature into broad service. Its intended missions included troop movement, casualty evacuation, reconnaissance, training, and special-purpose transport. That makes the design relevant even without mass deployment: it shows a capability requirement that older Soviet helicopter families did not fully satisfy. For an equipment page, the correct framing is a promising but delayed program with influence on related civil and utility helicopter development rather than a proven operational fleet type.

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