Дмитриев В. П.: Х-11
Dmitriev V. P.: X-11

General data

Producer info

Pictures

Video clips

Data sources

Names and dates
Market original model designation
Х-11
Market model designation (english translation or spelling)
X-11
Date of prototype completion
1961
Tests start date
1961
(...)
1976-12
Country of manufacture
Kyrgyzstan
(...)
Ukraine
People involved
P. Mikalyukin {П. Микалюкин}Constructor
Vladimir Mikalyukin {Владимир Микалюкин}Helper
Config info
Rotorcraft typeHelicopter
Config
Coaxial rotors
Weights
Maximum Takeoff Weight (MTOW)
350
kg
Manufacturers empty weight (MEW)
270
kg
Cabin and cockpit
Maximum number of people onboard
1
Main rotor
Main rotor diameter
6.50
m
Number of blades
2
Powerplant
Engine model
Татраплан-600
Engine model (english translation or spelling)
Tatraplan-600
Engine type
Piston
Engine dry weight
60
kg
Number of engines
1
Total maximum power
62
HP
Angular speed at max power
4500
rpm
0.0525