Войтович С. П.
Voytovich S. P.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Date of prototype completion
1974
First flight date and time
1974-12
Country of manufacture
Ukraine
People involved
Sergei Voytovich {Сергей Войтович}Chief design engineer, Test pilot
Config info
Rotorcraft typeGyroglider
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
Landing gear type
Wheeled
Wheeled landing gear type
Main wheels in the back
Landing gear support points
3
Main landing gear wheel diameter
0.30
m
Main landing gear shock absorption type
No translation available for: ldg_shock_abs_none
Nose landing gear wheel diameter
0.30
m
Nose landing gear shock absorption type
No translation available for: ldg_shock_abs_none
Control system
Max forward tilt of main rotor axis
16
°
Max rearward tilt of main rotor axis
16
°
Max left tilt of main rotor axis
16
°
Max right tilt of main rotor axis
16
°
Rudder left deflection
25
°
Rudder right deflection
25
°
Main rotor
Main rotor type
Rigid
Main rotor diameter
6.10
m
Pre-coning angle
4
°
Preset blade incidence angle
2
°
Main rotor blade chord
0.18
m
Main rotor blade airfoil
NACA 23012
Performance
Take-off speed
36
km/h
0.0932