SLIUSARIEV, V.; BUCHARSKYI, V. Development of a mathematical model for the cooling channel of a liquid propellant rocket engine’s chamber with respect for variations in coolant density. Eastern-European Journal of Enterprise Technologies, [S. l.], v. 6, n. 1 (132), p. 14–20, 2024. DOI: 10.15587/1729-4061.2024.316236. Disponível em: https://journals.uran.ua/eejet/article/view/316236. Acesso em: 6 dec. 2025.