Kamov

Ka-26 family

The Ka‑26 family, produced by the Russian helicopter manufacturer Kamov, entered service in the early 1960s as a versatile, twin‑engine, coaxial‑rotor utility aircraft. Designed under the leadership of Nikolai Kamov, the first prototype flew on 28 March 1960 and the type was introduced to the Soviet civil and military fleets in 1965. Its most distinctive feature is the coaxial rotor system, which eliminates the need for a tail rotor, providing compact dimensions, high maneuverability and excellent hover performance in confined areas. Powered by two Ivchenko AI‑14V radial engines, the Ka‑26 can be equipped with interchangeable pod‑type cabins for cargo, passenger, ambulance, agricultural spraying or firefighting missions, making it a true modular platform. The aircraft’s rugged airframe, simple maintenance requirements and short take‑off and landing capabilities allowed operation from unprepared fields, riverbanks and ship decks, contributing to its widespread use in remote regions of the USSR and later Russia, as well as in several foreign air services. Over 2,000 units were built, and the Ka‑26’s design principles influenced later Kamov models such as the Ka‑32, confirming its lasting impact on coaxial‑rotor aviation.

Classification

Dimensions

Length
7.75 metre

Production & History

First Flight
1965
Service Entry
1969

Design & Classification

Manufacturer
Kamov
Designer
Kamov
NATO Name
Hoodlum
Engine
Omsk TVO-100
Operator
Lithuanian State Border Guard Service Gazprom Avia Hungarian Air Force Bulgarian Air Force
Wikidata ID
Q1043860