Артемчук Я.: А-2
Artemchuk Y.: A-2

General data

Producer info

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Names and dates
Market original model designation
А-2
Market model designation (english translation or spelling)
A-2
Date of prototype completion
1966
Tests start date
1967
Country of manufacture
Ukraine
People involved
Yakov Artemchuk {Яков Артемчук}Constructor
Vasily Artemchuk {Васили Артемчук}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
160
kg
Manufacturers empty weight (MEW)
80
kg
Cabin and cockpit
Maximum number of people onboard
1
Control system
Max forward tilt of main rotor axis
0
°
Max rearward tilt of main rotor axis
30
°
Max left tilt of main rotor axis
10
°
Max right tilt of main rotor axis
10
°
Main rotor
Cyclic control
Tilting rotor shaft
Collective control
Yes
Main rotor diameter
6
m
Number of blades
2
Minimum collective pitch angle
-15
°
Maximum collective pitch angle
15
°
Autodynamic hub’s flapping hinge angle
30
°
Main rotor blade chord
0.21
m
Powerplant
Engine model
Д-300
Engine model (english translation or spelling)
D-300
Engine type
Piston
Number of engines
1
Total maximum power
30
HP
0.0782