Samara University Repository
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This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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| Title: | Лазерный ракетный двигатель непрерывного действия с множественными плазменными образованиями в камере поглощения |
| Authors: | Саттаров А. Г. |
| Keywords: | continuous optical discharge fiber lasers jet propulsion laser rocket engines laser stands multiple plasma formations specific impulse волоконные лазеры лазерные ракетные двигатели лазерные стенды множественные плазменные образования непрерывный оптический разряд реактивная тяга удельный импульс |
| Issue Date: | 2025 |
| Citation: | Саттаров, А. Г. Лазерный ракетный двигатель непрерывного действия с множественными плазменными образованиями в камере поглощения = Continuous laser rocket engine with multiple plasma formations organized in the absorption chamber / А. Г. Саттаров // 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. 1033-1035. |
| Abstract: | This paper presents the results of research on the development of laser rocket engines based on continuous optical discharge with the formation of multiple plasma formations in the absorption chamber along the propagation of one laser beam. The proposed method for organizing the working process in the chamber increases the efficiency of a continuous rocket engine as a result of increasing the share of absorbed laser radiation energy when it passes through several plasma formations. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43406 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-1033-1035.pdf | 472.82 kB | Adobe PDF | View/Open |
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