Technical data
Type Ka-10
Function Observation, liaison
Year 1949
Crew 1
Engines 1*55hp AI-4V
Rotor diameter 6.1m
Length ?
Width (with rotors) ?
Empty weight 234kg
Loaded weight 375kg
Rotor (disk) load 12.75
Power load (kg/hp) 6.82
Maximum Speed 90km/h
Static Ceiling 500m
Dynamic Ceiling 1000m
Range 95

Ka-10, N.I.Kamov 'Hat'

The Ka-10 in flight. 16k b/w photo from the "History of aircraft construction in the USSR" Vol.2 , p.444

Development of the Ka-8, same general layout but bigger. Its AI-4V engine was the second in the USSR (after AI-26GR) specially designed for helicopters. Flight control system was almost same as on the Ka-8.

12 built, used for research and demonstration.

Precursor: Ka-8.


Sources [6], Vol.2 p.442;

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