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: | experimental research laser radiation intensity numerical modeling orientation and stabilization systems point explosion pulsed laser rocket engines pulsed optical discharge shock waves small spacecraft импульсные лазерные ракетные двигатели импульсный оптический разряд интенсивность лазерного излучения малые космические аппараты системы ориентации и стабилизации точечный взрыв ударная волна численное моделирование экспериментальные исследования |
| 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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