Effect of thermal instability factors on the hydraulic characteristics of the capillary injector element liquid rocket thrusters
Автор: Nigodjuk Valentin, Sulinov Alexander
Журнал: Известия Самарского научного центра Российской академии наук @izvestiya-ssc
Рубрика: Механика и машиностроение
Статья в выпуске: 6-4 т.15, 2013 года.
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By calculation and theoretical study of the influence of thermal factors on the hydraulic characteristics of the capillary injector element liquid rocket thrusters. It is shown that the influence of thermal factors can lead to significant changes in the hydraulic characteristics of injector components of rocket engine thrust of 1 N and, consequently, to the instability of the engine and its nonisobaric work.
Rocket thrusters, air washers capillary elements hydraulics, thermal factors, instability parameters
Короткий адрес: https://sciup.org/148202666
IDR: 148202666
