Авторы: Arkhipov V.A., Bondarchuk S.S., Zhukov A.S., Zolotorev N.N., Perfil’eva K.G.
Название публикации: Performance optimization of a standard-flow hybrid rocket engine
Название источника: Combustion Explosion And Shock Waves
Библиографическая ссылка: Arkhipov V.A., Bondarchuk S.S., Zhukov A.S., Zolotorev N.N., Perfil’eva K.G. Performance optimization of a standard-flow hybrid rocket engine // Combustion Explosion And Shock Waves. - 2017. - Vol.53. - Iss.6. - P.634-640.
Библиографическая ссылка2: Arkhipov, V.A., Bondarchuk, S.S., Zhukov, A.S. et al. Combust Explos Shock Waves (2017) 53: 634. https://doi.org/10.1134/S001050821706003X
Ссылки: DOI: 10.1134/S001050821706003X; WoS: 000418838000003; SCOPUS: 2-s2.0-85039432447; РИНЦ: 32294941;
Реферат: 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.
Ключевые слова: hybrid rocket engine, solid propellant charge, additional oxidizer, burning rate, combustion efficiency
Год опуликования: 2017
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