Шевко С. В.
Shevko S. V.

General data

Producer info

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Data sources

Names and dates
Project start date
1989
Country of manufacture
Ukraine
People involved
Sergey Shevko {Сергей Шевко}Constructor
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Counteracting torque not required
Weights
Maximum Takeoff Weight (MTOW)
150
kg
Manufacturers empty weight (MEW)
60
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Length
2.05
m
Width
1.20
m
Height
1.95
m
Main rotor
Collective control
No
Main rotor diameter
6.35
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Preset blade incidence angle
4
°
Propeller
Mode
Pushing
Propeller diameter
0.40
m
Angular speed at max thrust
13000
rpm
Powerplant
Engine model
Vikhr-30
Engine type
Piston
Engine dry weight
18
kg
Total maximum power
28
HP
Angular speed at max power
5000
rpm
Fuel system
Fuel tank capacity
15
l
Performance
Maximum horizontal flight speed (Vh)
130
km/h
Best rate of climb
4
m/s
Maximum range
100
km
0.0413