Kamov Ka-26
Development of the Russian light multipurpose helicopter, the Ka-26 (NATO designation: 'Hoodlum'), began in 1962. The removable cabin is capable of carrying either six passengers or 2 stretchers and 3 seats; when removed, a cargo platform or sling can be fitted. Maximum internal and slung loads are 700 kg and 1000 kg, respectively.
.jpg "The Kamov Ka-26 taking flight.
Taken 14 October 2012, 14:04. Photo by Dmitry Terekhov from Odintsovo, Russian Federation.")
Overview
Data on design, manufacture and statusDesign authority: Kamov Design Bureau
Primary manufacturer: Kamov
Parent type: Kamov Ka-26
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Single seater arrangement
Landing gear: Wheels (non-retractable)
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used1999 (page 274)
Book
2000 (page 51)
Book
