Cicaré CH-11C
A single-seat, counter-rotating ultra-light helicopter designed back in 1998. 2014 installation of autonomous control systems has converted it into a UAV. It allows the adaptation of an additional piston engine and and also a turbine engine.
Overview
Data on design, manufacture and statusDesign authority: Cicaré S.A.
Primary manufacturer: Cicaré S.A.
Parent type: No type defined
Aircraft status: In development
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Single seater arrangement
Landing gear: Skids
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
Helicopter Cicare CH-11. Specifications. A photo. Подробнее на: http://en.avia.pro/blog/vertolyot-cicare-ch-11-tehnicheskie-harakteristiki-foto
N/A
http://en.avia.pro/blog/vertolyot-cicare-ch-11-tehnicheskie-harakteristiki-foto, January 10, 2017
Website
http://en.avia.pro/blog/vertolyot-cicare-ch-11-tehnicheskie-harakteristiki-foto, January 10, 2017
Website
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