Лопатченко В. Н.: Кондор
Lopatchenko V. N.: Condor

General data

Producer info

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Data sources

Names and dates
Market original model designation
Кондор
Market model designation (english translation or spelling)
Condor
Date of prototype completion
1986
People involved
V. Lopatchenko {В. Лопатченко}Constructor
Vladimir Lopatchenko {Владимир Лопатченко}Helper
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
286
kg
Manufacturers empty weight (MEW)
200
kg
Main rotor
Main rotor diameter
6.15
m
Main rotor blade chord
0.18
m
Main rotor blade airfoil
NACA 23012
Propeller
Propeller diameter
1.10
m
Thrust
834
N
Angular speed at max thrust
4000
rpm
Powerplant
Engine model
ZMZ-40 {ЗМЗ-40}
Total maximum power
40
HP
0.0487