Kamov Ka-10
Light single-seat coaxial helicopter developed by the Kamov Design Bureau in 1949; there is no fuselage. NATO Designation of the Kamov Ka-10 is Hat.
Overview
Data on design, manufacture and statusDesign authority: Kamov Design Bureau
Primary manufacturer: Kamov
Parent type: Kamov Ka-10
Aircraft status: No longer flying
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Single seater arrangement
Landing gear: Floats
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
OKB N.I.Kamova
G.I. Kuznetsov
1999 (page 156)
Book
1999 (page 156)
Book
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