Flight Test Demonstration of an Unducted Engine Architecture for SMR Aircraft

HORIZON-JU-CLEAN-AVIATION-2025-03-SMR-02

Flight test demonstration of an installed Open Fan engine architecture at TRL6 to demonstrate a -20% of CO2 reduction at aircraft level and demonstration up to TRL 5 of enhanced performance technologies and advanced modelling capabilities for further efficiency and fuel burn improvements. See the topic description document published with this call for full details.
Technical topics
G. Propulsion - G1. Endothermic Systems
G. Propulsion - G2. Green Propellant and Combustion
K. Integrated Design and Validation
L. Integrated Systems Technology
O. Operating Environment Technology
N. Innovative concepts and scenarios

HORIZON-JU-CLEAN-AVIATION

Deadline:

Call type: European

Max duration: 100M

Budget (per project): 48.00m€

TRL(end): 6

Eligible structures
Association/Network
Cluster
Intermediate Sized Enterprise
Large Company
Research and Technical Organisation
Small-Medium Enterprise
University
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