Храпчун Т. В.
Khrapchun T. V.

General data

Producer info

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Data sources

Names and dates
Project start date
1984
Date of prototype completion
1989
Country of manufacture
Ukraine
People involved
Taras Khrapchun {Тара­с Храпчун}Constructor
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Tail rotor
Weights
Maximum Takeoff Weight (MTOW)
300
kg
Cabin and cockpit
Maximum number of people onboard
2
External dimensions
Height
2.10
m
Main landing gear wheel diameter
0.28
m
Main landing gear wheel width
0.10
m
Nose landing gear wheel diameter
0.28
m
Nose landing gear wheel width
0.10
m
Main rotor
Cyclic control
Swash-plate (direct)
Collective control
Yes
Main rotor diameter
7
m
Number of blades
2
Main rotor blade mass
13
kg
Tail rotor
Tail rotor diameter
1
m
Number of blades
2
Tail rotor blade chord
0.11
m
Powerplant
Engine model
Cezet 400
Number of engines
2
Total maximum power
84
HP
0.0562