Войтович С. П.
Voytovich S. P.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Project start date
1998
Country of manufacture
Ukraine
People involved
Sergei Voytovich {Сергей Войтович}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
200
kg
External dimensions
Length
3.10
m
Width
1.80
m
Height
2.10
m
Main landing gear wheel diameter
0.28
m
Main landing gear wheel width
0.09
m
Nose landing gear wheel diameter
0.28
m
Nose landing gear wheel width
0.09
m
Main rotor
Main rotor type
Semi-rigit
Main rotor diameter (System no.: 1)
7
m
Main rotor diameter (System no.: 2)
3
m
Preset blade incidence angle (System no.: 1)
4
°
Preset blade incidence angle (System no.: 2)
4
°
Main rotor blade chord (System no.: 1)
0.22
m
Main rotor blade chord (System no.: 2)
0.30
m
Main rotor blade airfoil (System no.: 1)
NACA 8-H-12
Main rotor blade airfoil (System no.: 2)
NACA 0015
Propeller
Propeller diameter
1.05
m
Thrust
686
N
Powerplant
Engine model (System no.: 1)
Вихрь-30
Engine model (english translation or spelling) (System no.: 1)
Vikhr 30
Engine model (System no.: 2)
Ветерок-8
Engine model (english translation or spelling) (System no.: 2)
Veterok-8
Total maximum power
38
HP
Angular speed at max power (System no.: 1)
5000
rpm
Angular speed at max power (System no.: 2)
4800
rpm
Fuel system
Aux fuel tank capacity
10
l
Performance
Maximum horizontal flight speed (Vh)
100
km/h
Best rate of climb
2
m/s
Miminum rate of descend in autorotation
2
m/s
0.114