Яшин А. Р.
Yashin A. R.

General data

Producer info

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Data sources

Names and dates
Project start date
1987
Project end date
1990
People involved
Andrei Yashin {Андрей Яшин}Chief design engineer
S. Ryabikov {С. Рябиков}Project supervisor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
220
kg
Manufacturers empty weight (MEW)
117
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Landing gear track
1.60
m
Main landing gear wheel diameter
0.28
m
Main landing gear wheel width
0.10
m
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.20
m
Number of blades
2
Main rotor blade chord
0.18
m
Propeller
Propeller diameter
1.60
m
Thrust
1422
N
Powerplant
Engine model
Manuylenko {Мануйленко}
Engine type
Piston
Number of engines
1
Total maximum power
56
HP
Fuel system
Fuel tank capacity
33
l
Performance
Maximum horizontal flight speed (Vh)
140
km/h
Cruise speed (Vc)
82
km/h
Take-off speed
35
km/h
Take-off distance
85
m
Landing speed
16
km/h
Landing distance
8
m
Best rate of climb
6
m/s
Best glide ratio
3.6
0.1085