Войтович С. П.
Voytovich S. P.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Date of prototype completion
1977
Tests start date
1977-12
First flight date and time
1978
Country of manufacture
Ukraine
People involved
Sergei Voytovich {Сергей Войтович}Design engineer, Test pilot
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
190
kg
Manufacturers empty weight (MEW)
100
kg
External dimensions
Length
3.20
m
Width
1.70
m
Height
2
m
Landing gear type
Wheeled
Main landing gear wheel diameter
0.29
m
Main landing gear shock absorption type
No translation available for: ldg_shock_abs_bend_elas_elem
Nose landing gear wheel diameter
0.29
m
Control system
Lateral control
Main rotor
Longitudinal control
Main rotor
Max forward tilt of main rotor axis
16
°
Max rearward tilt of main rotor axis
16
°
Max left tilt of main rotor axis
12
°
Max right tilt of main rotor axis
12
°
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.60
m
Preset blade incidence angle
2
°
Flapping hinge offset
0.22
m
Max flapping angle (up)
5
°
Max flapping angle (down)
5
°
Propeller
Propeller diameter
1
m
Thrust
441
N
Powerplant
Engine model
ПД-10
Engine model (english translation or spelling)
PD-10
Engine type
Piston
Number of engines
1
Total maximum power
17
HP
Angular speed at max power
4200
rpm
Fuel system
Fuel tank capacity
12
l
Performance
Take-off speed
50
km/h
0.1168