Панасевич В. Н.
Panasevich V. N.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Date of prototype completion
1989
Country of manufacture
Ukraine
People involved
Victor Panasevich {Виктор Панасевич}Constructor, Test pilot
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
160
kg
Manufacturers empty weight (MEW)
90
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Main landing gear wheel diameter
0.28
m
Main landing gear wheel width
0.09
m
Nose landing gear wheel diameter
0.28
m
Nose landing gear wheel width
0.09
m
Control system
Lateral control
None
Longitudinal control
Main rotor
Main rotor
Main rotor type
Rigid
Cyclic control
Tilting rotor shaft
Main rotor diameter
5
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Main rotor blade chord
0.22
m
Main rotor blade twist
0
°
Propeller
Mode
Pushing
Propeller diameter
1
m
Propeller direction of rotation
Clockwise
Number of blades
2
Powerplant
Engine model
PD-10/IZ
Engine type
Piston
Engine dry weight with propeller
30
kg
Number of engines
1
Total maximum power
18
HP
Angular speed at max power
4800
rpm
Static thrust
490
N
Performance
Take-off speed
50
km/h
0.1118