Deadline: 2026-05-19 Status: Future Opening
Description
Expected Outcome:Development and demonstration of a low power Ice Protection System for the wing and empennage of an Ultra-Efficient Regional Aircraft concept based on hybrid-electric propulsion. The topic covers ground demonstrations to TRL5 representative of EASA CS-25 icing conditions and targets a lightweight and low drag solution compatible with regional aircraft non-propulsive power levels. See the topic description document published with this call for full details.
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