Камов: Ка-10 Иркутянин
Kamov: Ka-10 Irkutyanin

General data

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Names and dates
Market original model designation
Ка-10
Market model designation (english translation or spelling)
Ka-10
Original model name
Иркутянин
Model name (english translation or spelling)
Irkutyanin
Project start date
1948-10-07
Date of prototype completion
1949
First flight date and time
1949-08-30
Country of manufacture
Russia
People involved
Nikolai Kamov {Николай Камов}Chief design engineer
A. Konradov {А. Конрадов}No translation available for: func_engineer
V. Biryulin {В. Бирюлин}No translation available for: func_engineer
V. Zakharyin {В. Захарьин}No translation available for: func_engineer
Mikhail Gurov {Михаил Гуров}Test pilot
D. Efremov {Д. Ефремов}Test pilot
Yefim Kedrovsky {Ефим Кедровский}Test pilot
V. Barshevsky {В. Баршевский}Function unknown
M. Kupfer {М. Купфер}Function unknown
A. Vlasenko {А. Власенко}Function unknown
Config info
Rotorcraft typeHelicopter
Config
Coaxial rotors
Weights
Maximum Takeoff Weight (MTOW)
370
kg
Manufacturers empty weight (MEW)
239
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Fuselage length
3.90
m
Fuselage width
2
m
Fuselage height
2.50
m
Control system
Lateral control
Main rotor
Longitudinal control
Main rotor
Yaw control
Main rotors differential torque
Main rotor
Main rotor type
Fully articulated
Cyclic pitch control
Yes
Collective control
Yes
Main rotor diameter
5.80
m
Number of blades
3
Main rotor blade airfoil
NACA 23012
Main rotor blade twist
5
°
Powerplant
Engine model
АИ-4-Г (AI-4-G)
Engine type
Piston
Number of engines
1
Total maximum power
55
HP
Angular speed at max power
4200
rpm
Fuel system
Aux fuel tank capacity
33
l
Performance
Maximum horizontal flight speed (Vh)
115
km/h
Maximum service ceiling
2500
m
Hover ceiling OGE
300
m
Maximum range
120
km
Maximum flight endurance
1.20
h
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