Email this article Performance optimization of a standard-flow hybrid rocket engine
- Authors: 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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Affiliations:
- Tomsk State University
- Institute for Problems of Chemical and Energetic Technologies, Siberian Branch
- Issue: Vol 53, No 6 (2017)
- Pages: 634-640
- Section: Article
- URL: https://journals.rcsi.science/0010-5082/article/view/152983
- DOI: https://doi.org/10.1134/S001050821706003X
- ID: 152983
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Abstract
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.
About the authors
V. A. Arkhipov
Tomsk State University
Author for correspondence.
Email: leva@niipmm.tsu.ru
Russian Federation, Tomsk, 634050
S. S. Bondarchuk
Institute for Problems of Chemical and Energetic Technologies, Siberian Branch
Email: leva@niipmm.tsu.ru
Russian Federation, Biisk, 659322
A. S. Zhukov
Tomsk State University
Email: leva@niipmm.tsu.ru
Russian Federation, Tomsk, 634050
N. N. Zolotorev
Tomsk State University
Email: leva@niipmm.tsu.ru
Russian Federation, Tomsk, 634050
K. G. Perfil’eva
Tomsk State University
Email: leva@niipmm.tsu.ru
Russian Federation, Tomsk, 634050
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