01.1 - Aircraft Design and Integrated System (Basics and Theory)
CRYOGENIC TANK SIZING MODEL FOR THE CONCEPTUAL DESIGN OF HYDROGEN-POWERED AIRCRAFT
G. Licheva¹, S. Liscouët-Hanke¹; ¹Concordia University, Canada
This paper presents a parametric model for cryogenic hydrogen tanks for aircraft conceptual design in an MDAO context. The model considers hydrogen properties, filling pressure, tank geometry, insulation, and installation constraints. Case studies for various tank installation and configuration scenarios are presented for a notional business aircraft, considering aircraft-level impact.