Samara University Repository
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| Title: | Импульсный лазерный ракетный двигателей для систем ориентации и стабилизации малых космических аппаратов |
| Authors: | Саттаров А. Г. Кононенко О. Д. Бикмучев А. Р. Сочнев А. В. Зиганшин Б. Р. |
| Keywords: | orientation and stabilization systems numerical modeling laser radiation intensity experimental research импульсные лазерные ракетные двигатели экспериментальные исследования численное моделирование ударная волна точечный взрыв системы ориентации и стабилизации малые космические аппараты интенсивность лазерного излучения импульсный оптический разряд small spacecraft shock waves pulsed optical discharge pulsed laser rocket engines point explosion |
| Issue Date: | 2025 |
| Citation: | Импульсный лазерный ракетный двигателей для систем ориентации и стабилизации малых космических аппаратов = Pulse laser rocket engine for small space vehicles orientation and stabilization systems / А. Г. Саттаров, О. Д. Кононенко, А. Р. Бикмучев, А. В. Сочнев, Б. Р. Зиганшин // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 1024-1027. |
| Abstract: | In this paper, the authors propose using a pulsed laser rocket engine as an alternative option for performing orientation and stabilization tasks for small spacecraft, based on obtaining a near-surface pulsed optical discharge in a cylindrical absorption chamber in a working gas medium, such as air. The results of numerical calculation of the characteristics of this type of pulsed laser rocket engine are presented using the equations of the Sedov-Taylor point explosion theory. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43263 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-1024-1027.pdf | 462.62 kB | Adobe PDF | View/Open |
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