Комета: Комета-1
Kometa: Kometa-1

General data

Producer info

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Names and dates
Market original model designation
Комета-1
Market model designation (english translation or spelling)
Kometa-1
Project start date
1993
Date of prototype completion
1994
Country of manufacture
Ukraine
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
160
kg
Manufacturers empty weight (MEW)
80
kg
External dimensions
Length
2.90
m
Width
1.50
m
Height
2.02
m
Main rotor
Cyclic control
Tilting rotor shaft
Main rotor diameter
6.30
m
Number of blades
2
Main rotor blade chord
0.18
m
Main rotor blade airfoil
NACA 8-H-12
Propeller
Propeller diameter
1.20
m
Number of blades
2
Propeller material
Wood
Thrust
785
N
Powerplant
Engine model
MP-800 / IZ-P-3
Engine type
Piston
Total maximum power
36
HP
0.0972