Aircraft Liquid Hydrogen Fuel Distribution System Technologies for Direct Burn Applications

Design and development of the aircraft liquid hydrogen fuel distribution system components for Hydrogen Direct Burn Propulsion Systems (modelling & simulation, up to ground demonstration of full functional system at TRL6 by end of Phase 1).
Technical topics
A. Flight physics - A1. Aerodynamics
D. Device Technology
G. Propulsion - G2. Green Propellant and Combustion
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): 10.00m€

TRL(end): 5

Eligible structures
Intermediate Sized Enterprise
Large Company
Research and Technical Organisation
Small-Medium Enterprise
University
Have feedback or updates for this entry?