Mathematical model of the propellant tank pressurization system with respect of heat exchange
Mathematical model of the propellant tank pressurization system with respect of heat exchange Vitalii Alieksieienko ORCID: https://orcid.org/0009-0000-8317-0096 Oles Honchar Dnipro National University Valerii Bucharskyi ORCID: https://orcid.org/0000-0002-8245-5652 Oles Honchar Dnipro National University The pressurization system for launch vehicle fuel tanks is designed to maintain excess pressure in the gas cushion of the tanks according to the calculated dependency, determined by the requirements for the supply of fuel components and the tank design. To achieve this, it is necessary to coordinate the …