Multi-MW Fuel Cell Propulsion System for Hydrogen-Powered Aircraft

Design & Integration Optimisation of a Full Electric Large Scale Multi-MW (~3MW) Fuel Cell HIPS (Hydrogen Integrated Propulsion System) based on an aviation-grade Fuel Cell for Regional Aircraft Applications up to system/sub-system validation at TRL4 by end of Phase 1.
Technical topics
B. Manufacturing Processes/Design Tools/Techniques
D. Device Technology
G. Propulsion - G2. Green Propellant and Combustion
G. Propulsion - G3. Electric Systems
H. Avionics and On-board Systems - H4. Major s/s

Horizon Europe - Clean Aviation Joint Undertaking

Deadline:

Call type: European

Max duration: 36M

Budget (per project): 35.00m€

TRL(end): 5

Eligible structures
Intermediate Sized Enterprise
Large Company
Research and Technical Organisation
Small-Medium Enterprise
University
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