Performance optimization of a standard-flow hybrid rocket engine

V. A. Arkhipov; S. S. Bondarchuk; A. S. Zhukov; N. N. Zolotorev; K. G. Perfil’eva

doi:10.1134/S001050821706003X

Performance optimization of a standard-flow hybrid rocket engine

作者: Arkhipov V.A.¹, Bondarchuk S.S.², Zhukov A.S.¹, Zolotorev N.N.¹, Perfil’eva K.G.¹
隶属关系:
1. Tomsk State University
2. Institute for Problems of Chemical and Energetic Technologies, Siberian Branch
期: 卷 53, 编号 6 (2017)
页面: 634-640
栏目: Article
URL: https://journals.rcsi.science/0010-5082/article/view/152983
DOI: https://doi.org/10.1134/S001050821706003X
ID: 152983

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详细

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.