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 status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 2 in Coaxial configuration

Crew required: 1 in Single seater arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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Related Public Resources

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