Отправить статью по E-mail Performance optimization of a standard-flow hybrid rocket engine
- Авторы: Arkhipov V.A.1, Bondarchuk S.S.2, Zhukov A.S.1, Zolotorev N.N.1, Perfil’eva K.G.1
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Учреждения:
- Tomsk State University
- Institute for Problems of Chemical and Energetic Technologies, Siberian Branch
- Выпуск: Том 53, № 6 (2017)
- Страницы: 634-640
- Раздел: Article
- URL: https://journals.rcsi.science/0010-5082/article/view/152983
- DOI: https://doi.org/10.1134/S001050821706003X
- ID: 152983
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Аннотация
A method for performance optimization of a standard-flow hybrid rocket engine is considered. The method is based on inserting an additional amount of an oxidizer into a solid propellant with a prescribed distribution of the oxidizer mass fraction along the solid propellant charge. An analytical dependence is derived for the oxidizer fraction distribution that ensures uniform combustion and high efficiency of the solid propellant charge.
Об авторах
V. Arkhipov
Tomsk State University
Автор, ответственный за переписку.
Email: leva@niipmm.tsu.ru
Россия, Tomsk, 634050
S. Bondarchuk
Institute for Problems of Chemical and Energetic Technologies, Siberian Branch
Email: leva@niipmm.tsu.ru
Россия, Biisk, 659322
A. Zhukov
Tomsk State University
Email: leva@niipmm.tsu.ru
Россия, Tomsk, 634050
N. Zolotorev
Tomsk State University
Email: leva@niipmm.tsu.ru
Россия, Tomsk, 634050
K. Perfil’eva
Tomsk State University
Email: leva@niipmm.tsu.ru
Россия, Tomsk, 634050
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