Войтович С. П.
Voytovich S. P.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Date of prototype completion
1975
First flight date and time
1975
Country of manufacture
Ukraine
People involved
Sergei Voytovich {Сергей Войтович}Chief design engineer, Test pilot
Config info
Rotorcraft typeGyroglider
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
120
kg
Manufacturers empty weight (MEW)
45
kg
External dimensions
Length
3
m
Width
1.60
m
Height
1.95
m
Control system
Rudder left deflection
25
°
Rudder right deflection
25
°
Main rotor
Main rotor type
Semi-rigit
Main rotor diameter
6.10
m
Number of blades
2
Pre-coning angle
4
°
Main rotor blade tip chord
0.18
m
Main rotor blade mass
5.50
kg
Performance
Take-off speed
36
km/h
0.1113