Сауткин А. А.
Sautkin A. A.

General data

Producer info

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Names and dates
Date of prototype completion
1992
First flight date and time
1993-05-29
Country of manufacture
Russia
People involved
Alexander Sautkin {Александр Сауткин}Constructor
Config info
Rotorcraft typeGyroglider
Weights
Maximum Takeoff Weight (MTOW)
170
kg
Manufacturers empty weight (MEW)
100
kg
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.40
m
Prerotation
Yes
Prerotation type
Drum and rope
Main rotor angular speed
420
rpm
Preset blade incidence angle
1.20
°
Main rotor blade twist
4.50
°
Main rotor blade mass
11.60
kg
Performance
Miminum towed speed
60
km/h
Maximum towed speed
110
km/h
Take-off speed
50
km/h
(...)
45
km/h
0.0611