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