Рисюк Ю. В.
Risyuk Yu. V.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Project start date
1990
Date of prototype completion
1991
First flight date and time
1991
Country of manufacture
Russia
People involved
Victor Shumeiko {Виктор Шумейко}Design engineer, Test pilot
A. Salikov {А. Саликов}Design engineer
A. Shustov {А. Шустов}Design engineer
Yu. Risyuk {Ю. Рисюк}Design engineer
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
210
kg
Manufacturers empty weight (MEW)
130
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Height
1.90
m
Landing gear track
1.60
m
Main landing gear wheel diameter
0.30
m
Main landing gear wheel width
0.13
m
Nose landing gear wheel diameter
0.20
m
Nose landing gear wheel width
0.08
m
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Main rotor diameter
5.70
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Propeller
Mode
Pushing
Propeller diameter
0.90
m
Thrust
883
N
Angular speed at max thrust
5500
rpm
Powerplant
Engine model
Ural
Number of engines
1
Total maximum power
28
HP
Performance
Best rate of climb
0.50
m/s
0.0607