Нелипюк Ю. В.
Nelipyuk Yu. V.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Project start date
1998
Date of prototype completion
1999
First flight date and time
1999-07-30
Country of manufacture
Ukraine
People involved
Yuri Nelipyuk {Юрий Нелипюк}Constructor
Leonid Kozyarchuk {Леонід Козярчук}Consultant
Viktor Yatsenyuk {Виктор Яценюк}Test pilot
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
240
kg
Manufacturers empty weight (MEW)
140
kg
External dimensions
Length
3.30
m
Width
1.80
m
Height
2.55
m
Wheelbase
1.70
m
Main landing gear wheel diameter
0.30
m
Main landing gear wheel width
0.13
m
Nose landing gear wheel diameter
0.30
m
Nose landing gear wheel width
0.13
m
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.20
m
Number of blades
2
Main rotor blade chord
0.18
m
Main rotor blade airfoil
NACA 8-H-12
Propeller
Propeller diameter
1.60
m
Thrust
1177
N
Powerplant
Engine model
МП-800Б / ИЖ-П-5
Engine model (english translation or spelling)
MP-800B / IZ-P-5
Engine type
Piston
Number of engines
1
Total maximum power
45
HP
Angular speed at max power
5000
rpm
Fuel system
Fuel tank capacity
30
l
0.0605