Куклин С. Н.
Kuklin S. N.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Project start date
1987
Date of prototype completion
1995
Tests start date
1995
Country of manufacture
Russia
People involved
Sergey Kuklin {Сергей Куклин}Constructor
Alexander Efimchev {Александр Ефимичев}Test pilot
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
320
kg
External dimensions
Main landing gear wheel diameter
0.40
m
Main rotor
Main rotor type
Semi-rigit
Main rotor diameter
7.30
m
(...)
6.40
m
Prerotation
No
Number of blades
2
Main rotor blade chord
0.21
m
(...)
0.18
m
Main rotor blade airfoil
NACA 4412
Propeller
Number of blades
2
Propeller material
Wood
Thrust
1079
N
Powerplant
Engine model
ИЖ-П-Спорт
Engine model (english translation or spelling)
IZ-P Sport
Engine type
Piston
Number of engines
1
Total maximum power
45
HP
Fuel system
Fuel tank capacity
40
l
0.098