Россия
Статья посвящена решению задачи оценки дополнительных микроускорений, возникающих в результате температурного удара при выходе малого космического аппарата из тени Земли и погружении в неё, с целью выработки рекомендаций по контролю уровня микроускорений в зоне размещения технологического оборудования, предназначенного для реализации гравитационно-чувствительных технологических процессов на борту малого космического аппарата
контактная механика инженерных поверхностей, трение и износ сопряжений, триботехническое материаловедение, механика и процессы управления, кинематика, динамика, прочность, надежность машин и элементов конструкций
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