Шевченко Ю. А.
Shevchenko Yu. A.

General data

Producer info

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Names and dates
Date of prototype completion
1986
Tests start date
1987
Country of manufacture
Russia
People involved
Yuri Shevchenko {Юрий Шевченко}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
180
kg
Manufacturers empty weight (MEW)
90
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Front landing gear track
1.60
m
Wheelbase
1.15
m
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6
m
Preset blade incidence angle
0
°
Main rotor blade chord
0.17
m
Main rotor blade airfoil
Kupfer
Propeller
Propeller diameter (option 1)
1.25
m
Propeller diameter (option 2)
1.40
m
Thrust (option 1)
843
N
Thrust (option 2)
1030
N
Powerplant
Engine model
Cezet 500 mod.
Engine dry weight
28
kg
Number of engines
1
Total maximum power
42
HP
Angular speed at max power
6600
rpm
Performance
Maximum horizontal flight speed (Vh)
115
km/h
Minimum speed
37
km/h
Take-off distance
50
m
Best rate of climb
3
m/s
Maximum service ceiling
3000
m
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