Клуб Ротор: Р-13М
Club Rotor: R-13M

General data

Producer info

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Names and dates
Market original model designation
Р-13М
Market model designation (english translation or spelling)
R-13M
Date of prototype completion
1995
First flight date and time
1997
Country of manufacture
Russia
People involved
V. Khribkov {В. Хрибков}Chief design engineer
A. Vlasov {А. Власов}Design engineer
N. Ismagilov {Н. Исмагилов}Design engineer
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
230
kg
Manufacturers empty weight (MEW)
120
kg
Main rotor
Collective control
No
Main rotor diameter
7.30
m
Main rotor blade chord
0.32
m
Main rotor blade airfoil
NACA 23012
Main rotor blade mass
7.50
kg
Propeller
Number of blades
3
Thrust
1128
N
Powerplant
Engine model
Буран
Engine model (english translation or spelling)
Buran
Total maximum power
28
HP
Performance
Maximum horizontal flight speed (Vh)
110
km/h
Minimum speed
40
km/h
Best rate of climb
1.50
m/s
0.0761