Панякин-Пашков
Panyakin-Pashkov

General data

Producer info

Pictures

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Data sources

Names and dates
Date of prototype completion
1973
First flight date and time
1973
Country of manufacture
Russia
People involved
Victor Panyakin {Виктор Па­някин}Constructor
Yuri Pashkov {Юрий Пашков}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Manufacturers empty weight (MEW)
130
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Nose landing gear wheel diameter
0.20
m
Nose landing gear wheel width
0.08
m
Control system
Lateral control
Main rotor
Longitudinal control
Main rotor
Yaw control
Rudder
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.10
m
Main rotor blade mass
7
kg
Propeller
Mode
Pushing
Propeller diameter
1.40
m
Thrust
1079
N
(...)
883
N
Transmission reduction ratio
1.8
Powerplant
Engine model
М-63
Engine model (english translation or spelling)
M-63
Number of engines
1
Total maximum power
36
HP
0.0563