Kutsar L. I.

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Project start date
1980
Country of manufacture
Estonia
People involved
Leonid KutsarDesign engineer, Test pilot
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Counteracting torque not required
Weights
Maximum Takeoff Weight (MTOW)
466
kg
Cabin and cockpit
Maximum number of people onboard
2
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
9.30
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Powerplant
Engine type
Ramjet
Engine dry weight
1.50
kg
Number of engines
2
Fuel system
Fuel type
Automotive, 95 Oct.
Average fuel consumption [volumetric]
84
l/h
Performance
Maximum horizontal flight speed (Vh)
80
km/h
Maximum flight endurance
0.67
h
0.0928