01.2 - Aircraft Design and Integrated Systems (Use cases and Applications)
ADVANCED MODELING AND ANALYSIS OF A LIQUID HYDROGEN SHORT-MEDIUM RANGE AIRCRAFT CONCEPT FOR 2035
M. Kotzem¹, J. Häßy¹, V. Kriewall Peters, Hamburg University of Technology (TUHH), Germany; P. Schatrow¹, S. Wöhler¹; ¹German Aerospace Center (DLR), Germany
This study contributes to the maturation of a conceptual LH2 aircraft by integrating results of high-fidelity simulations into the OAD process: a hydrogen specific engine model including preconditioning, an LH2 system architecture and on-board system topology, and a structural tank integration concept validated by crash simulations are introduced and the corresponding integration effects analysed.
DOI: 10.71945/icas2026_0333