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: | Предпосылки создания принципиальной схемы высокоэффективного воспламенительного устройства для ракетных двигателей малой тяги на несамовоспламеняющихся газожидкостных топливах |
| Authors: | Рыжков В. В. Лыкин А. Ю. |
| Keywords: | discharge cavity igniter devices ignition delays ignition systems low-thrust liquid rocket engines mixing chambers non-hyperigniting propellant components the autoignition process воспламенительные устройства задержки воспламенения камеры смешения несамовоспламеняющиеся компоненты топлива процесс самовоспламенения разрядная полость ракетные двигатели малой тяги системы воспламенения |
| Issue Date: | 2025 |
| Citation: | Рыжков, В. В. Предпосылки создания принципиальной схемы высокоэффективного воспламенительного устройства для ракетных двигателей малой тяги на несамовоспламеняющихся газожидкостных топливах = Prerequisites for the creation of a principal scheme of a highly efficient ignition device for low-thrust rocket engines on non-self- ignition gas-liquid fuels / В. В. Рыжков, А. Ю. Лыкин // 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. 1008-1009. |
| Abstract: | The paper describes the principal scheme of organization of the process of reliable ignition of non-self-igniting fuel compositions in conditions of a low-thrust rocket engine, in which part of the fuel ignites, and initiation of combustion of the main portion of the fuel in the combustion chamber from the combustion product flame formed in it. The proposed scheme will ensure reliable, multiple launch of low-thrust rocket engine with high dynamic characteristics. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43465 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-1008-1009.pdf | 271.59 kB | Adobe PDF | View/Open |
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