Share
Print
Call Updates
Jun 2, 2022 3:04:39 AM
Please note the following update:
Release 2 of the Questions and Answers Document has been uploaded.
Jun 2, 2022 3:04:38 AM
Please note that the following update:
Release 3 of the Questions and Answers Document has been uploaded.
May 4, 2022 4:16:54 PM
The submission session is now available for: HORIZON-JU-CLEAN-AVIATION-2022-01-TRA-01(HORIZON-JU-IA)
Apr 29, 2022 3:46:57 PM
Please note that the following updates:
A. Proposal Template:
B. Release 2 of the Questions and Answers Document has been uploaded
Apr 4, 2022 11:48:17 AM
Please note that the following documents have been added to this call in the Portal (see the relevant sections below):
A. Proposal Template Models:
B. Evaluation Forms for IA an RIA Actions - CA JU
C. Evaluation Form CSA Actions - CA JU
D. Release 1 of the Questions and Answers Document
Aircraft architectures & technology integration for aircraft concepts ranging from regional to short-medium range applications
TOPIC ID: HORIZON-JU-CLEAN-AVIATION-2022-01-TRA-01
Programme: Horizon Europe Framework Programme (HORIZON)
Call: Clean Aviation CfP 01 (HORIZON-JU-Clean-Aviation-2022-01)
Type of action: HORIZON-IA HORIZON Innovation Actions
Type of MGA: HORIZON Action Grant Budget-Based [HORIZON-AG]
Deadline model: single-stage
Planned opening date: 12 April 2022
Deadline date: 22 June 2022 17:00:00 Brussels time
Definition and detailed design studies of aircraft concepts and architectures targeting entry into service (EIS) by 2035. The configurations studied will aim at reducing fuel burn by at least 30% for SR/SMR aircraft and by 50% for Regional aircraft compared to 2020 state-of-the-art, seeking 100% SAF drop-in fuel compatibility. For concepts based on the use of hydrogen as fuel or energy source, the configurations studied will aim at no less than 15% reduction in aircraft energy demand compared to 2020 state-of-the-art. The design shall include the complete architecture layout (in terms of aircraft aerodynamic/structural configuration and propulsive/non-propulsive system architecture) up to a validated down-selected concept at project completion (including numerical simulations and wind tunnel tests where relevant).