02 - Systems Engineering and Integration
MODEL-BASED APPROACH FOR HYDROGEN PRELIMINARY AIRCRAFT DESIGN CONSIDERING SAFETY AND OPERABILITY
A. Sarr¹, J. Jézégou¹, P. de Saqui-Sannes¹; ¹ISAE-SUPAERO, France
This paper proposes a model based approach for system modelling and safety assessment for a tube-and-wing liquid hydrogen fuelled aircraft considering operability. System Engineering and Safety Assessment tools and methods are applied during the process. Initial analyses show that new functions need to be considered at aircraft and system levels since they would impact the preliminary design.