Зайцев И. В.
Zaitsev I. V.

General data

Producer info

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Names and dates
Date of prototype completion
1993
Tests start date
1993
People involved
I. Zaitsev {И. Зайцев}Chief design engineer
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
570
kg
Useful load
300
kg
Manufacturers empty weight (MEW)
270
kg
Cabin and cockpit
Maximum number of people onboard
2
External dimensions
Length
4.12
m
Width
2.03
m
Height
2.85
m
Main landing gear wheel diameter
0.30
m
Main landing gear wheel width
0.13
m
Nose landing gear wheel diameter
0.28
m
Nose landing gear wheel width
0.09
m
Main rotor
Collective control
Yes
Main rotor diameter
8.50
m
Main rotor direction of rotation
Counterclockwise
Prerotation
Yes
Prerotation type
Mechanical
Number of blades
2
Propeller
Mode (System no.: 1)
Pushing
Mode (System no.: 2)
Pushing
Propeller diameter (System no.: 1)
1.45
m
Propeller diameter (System no.: 2)
1.45
m
Propeller direction of rotation (System no.: 1)
Counterclockwise
Propeller direction of rotation (System no.: 2)
Clockwise
Number of blades (System no.: 1)
2
Number of blades (System no.: 2)
2
Powerplant
Engine model
M-18-02
Engine type
Piston
Total maximum power
110
HP
Angular speed at max power
7300
rpm
Fuel system
Fuel tank capacity
86
l
Performance
Maximum horizontal flight speed (Vh)
165
km/h
Cruise speed (Vc)
115
km/h
Maximum service ceiling
3000
m
Maximum flight endurance
4
h
0.1237