Kamov Ka-32
Development of the Russian Ka-32 (NATO Designation: 'Helix-C') began in 1980. The airframe, powerplant and rotor system are based on the Kamov Ka-27. Specifically, the Ka-32 is a civilian version of the SAR helicopter Ka-27PS. Maximum internal and slung loads are 3700 kg and 5000 kg, respectively.
Overview
Data on design, manufacture and statusDesign authority: Kamov Design Bureau
Primary manufacturer: Kamov
Parent type: Kamov Ka-32
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 3 in Side-by-side 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 used
Russia's Helicopter World
Vertolet
2000 (page 58)
Book
2000 (page 58)
Book
Russian Helicopters, Ka-27
Russian Нelicopters, JSC
5 July 2017 (page 181)
Website
5 July 2017 (page 181)
Website
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