Electro-Thermal Wing Ice Protection System For Large Aircraft

The Topic objective is to select partner who will support the Topic Manager for designing an electro-thermal wing ice protection system for large aircraft fully integrated in the leading edge and optimized regarding performance, reliability, maintainability, and reparability. The expected final maturity is TRL 5.

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Last update: 23 October 2018
Record number: 702151

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Permalink: https://cordis.europa.eu/programme/id/H2020_JTI-CS2-2015-CPW03-SYS-02-08

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