
In this paper it is shown the analysis of the onboard rocket tanks pressurization system functioning. The basic direction of the rocket tanks pressurization process are proposed.
Проведена оценка эффективности системы наддува баков. Рассмотрен вопрос оптимизации системы бортового наддува баков за счет использования вихревого энергоразделителя.
ДАВЛЕНИЕ, НАДДУВ, БАК, ИСПАРИТЕЛЬ, ДВИГАТЕЛЬ, ДРЕНАЖНО-ПРЕДОХРАНИТЕЛЬНЫЙ КЛАПАН, АГРЕГАТ РЕГУЛИРОВАНИЯ, ГАЗ НАДДУВА, КОМПОНЕНТ ТОПЛИВА, ВИХРЕВОЙ ЭНЕРГОРАЗДЕЛИТЕЛЬ
ДАВЛЕНИЕ, НАДДУВ, БАК, ИСПАРИТЕЛЬ, ДВИГАТЕЛЬ, ДРЕНАЖНО-ПРЕДОХРАНИТЕЛЬНЫЙ КЛАПАН, АГРЕГАТ РЕГУЛИРОВАНИЯ, ГАЗ НАДДУВА, КОМПОНЕНТ ТОПЛИВА, ВИХРЕВОЙ ЭНЕРГОРАЗДЕЛИТЕЛЬ
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