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Kamov KA-10

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General Data
Notes
First Flown
1949

Never went into production, was mostly a research and development platform.

NATO reporting name is HAT

Length
Height
Rotor Span
Lift Capability
Range
55 nm
Top Speed
48 kts
Empty Weight
234 kgs
Max Gross Weight
375 kgs
Service Ceiling
3,050 ft
Armament
n/a
Engines
1 Ivchenko AI-4V piston engine rated at 55 hp
Accommodations
1 pilot
Cargo
n/a
Operators
Similar Aircraft
none
Other Features
Landing gear consisted of floats

Kamov KA-10 Kamov KA-10 Kamov KA-10 Kamov KA-10 Kamov KA-10 Kamov KA-10

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