Мухин Г.
Mukhin G.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Approximated date of prototype completion
Late 1980's
Country of manufacture
Russia
People involved
Georgy Mukhin {Георгий Мухин}Project leader
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Manufacturers empty weight (MEW) without engine
72
kg
Cabin and cockpit
Maximum number of people onboard
1
Main rotor
Main rotor type
Fully articulated
Cyclic pitch control
Yes
Collective control
Yes
Main rotor diameter
6.50
m
Number of blades
3
Main rotor blade chord
0.14
m
Main rotor blade mass
4.50
kg
Main rotor hub mass with pitch links
9.25
kg
Powerplant
Engine model
Ural {Урал}
0.0921