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.
Design authority: Cicaré S.A.
Primary manufacturer: Cicaré S.A.
Parent type: No type defined
Aircraft status: In development
VTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Single seater arrangement
Landing gear: Skids