To design, develop and manufacture a demonstrator of Low Power De-Icing System, including the leading edge wing section where it will be installed. The demonstrator will be tested up to TRL 5 in a IWT (not part of this Topic); the Applicant shall also assure the support to testing activity for system performance validation. The system design will be based on the icing requirement of the regional aircraft wing to be provided by the Topic Manager. An Electro-Thermal de-ice solution would be preferred but the Applicant can propose alternative solutions. Please refer to the full and formal topic descriptions published in this call.