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 configuration: Coaxial (x2)

Crew required: 1

Crew seating: Single seater

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Rotax Rotax 912 reciprocating

Engine manufacturer: BRP-Powertrain GmbH & Co KG

Max continuous power: 100 kW (134 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 270 kg (595 lb)

Max Range: 210 km (113 nm)

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