Клуб Ротор: Р-13
Club Rotor: R-13

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
Р-13
Market model designation (english translation or spelling)
R-13
Date of prototype completion
1991
Tests start date
1992
Country of manufacture
Russia
People involved
A. Vlasov {А. Власов}Test pilot
Config info
Rotorcraft typeAutogyro
Config
Single rotor
Weights
Maximum Takeoff Weight (MTOW)
200
kg
Manufacturers empty weight (MEW)
105
kg
Cabin and cockpit
Maximum number of people onboard
1
Main rotor
Main rotor diameter
6.50
m
Number of blades
2
Minimum collective pitch angle
0
°
Maximum collective pitch angle
10
°
Main rotor blade chord
0.22
m
Main rotor blade airfoil
NACA 23012
Propeller
Mode
Pushing
Propeller diameter
1.60
m
Propeller direction of rotation
Counterclockwise
Number of blades
2
Thrust
883
N
Transmission reduction ratio
2.2
Powerplant
Engine model
RMZ-640
Number of engines
1
Total maximum power
28
HP
Performance
Maximum horizontal flight speed (Vh)
100
km/h
Minimum speed
60
km/h
Best rate of climb
1
m/s
0.0571