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Cicare CH-8
 
 Cicare-CH8-01
Cicare CH8
 
The objective of this project was to develop a two seat helicopter that fitted the ULM category, based on the platform of the Cicaré 7B and 7T, also to be sold as a kit.
 
The Cicaré 8 is built with aeronautical SAE 4130 chrome molybdenum steel and welded in spatial reticulated configuration and the cabin is a semi-monocoque made of composite carbon fiber and epoxy resin. The T-Shaped stabilizerhas a semi-monocoque type structure, built entirely in AL-2024 T3 and AL6061 T6.
 
Based on the ROTAX 900 series, with improved performance and features, the EPA POWER 917 is a block of Rotax engine with dual injection and carbon fiber components, which ensure a reliable and safe flight.
 
A semi-rigid, simple and optimum rotor, which is reflected in a soft and highly controllable helicopter. One highlight of the Cicare helicopters is the command system that was designed and patented by Augusto Cicaré under US PATENT: 5.165.854
 
 Cicare-CH8-02
 
The system ensures a smooth and seamless linkage between the engine and the transmission, allowing a gradual engagement which is almost imperceptible to the passengers in the cabin.
 
The kit price in 2021 was USD 121.500.
 
 Cicare-CH8-03
 
Engine: EPA R917 Ti, 135 hp
Empty Weight: 280 Kg (620lb)
MTOW: 480 Kg (1060lb)
VNE: 194 Km/h
Cruise speed: 150 km/h
Climb rate: 7 m/s / 1400 ft/min
Service Ceiling: 4500 m
Fuel: 95 octane
Endurance: 2,5 hrs
 
 Cicare-CH8-04
 
 
 
 


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