Thermal protection technologies for solid propellant rocket engines

Mironov, V. V.; Tolkach, M. A.; Timarov, A. G.

doi:10.31857/S0869587324070083

English

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Thermal protection technologies for solid propellant rocket engines

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Thermal protection technologies for solid propellant rocket engines

Annotation

PII

S0869587324070083-1

Publication type

Article

Status

Published

Authors

V. V. Mironov Send message

Affiliation: State Scientific Center of the Russian Federation “Keldysh Research Center”

M. A. Tolkach

Affiliation: State Scientific Center of the Russian Federation “Keldysh Research Center”

A. G. Timarov

Affiliation:
State Scientific Center of the Russian Federation “Keldysh Research Center”
Moscow Aviation Institute (Scientific Research University)

Edition

Volume 94 Issue number 7

Pages

677-687

Abstract

The article examines the thermal insulation characteristics of materials used in solid-fuel rocket engines manufactured in the United States, France, Italy, Japan, and other developed nations. The internal surfaces of combustion chambers in these rocket engines are subject to significant stress under thermo-mechanical loading conditions, necessitating specialized protection. The authors identify four categories of reinforced elastomeric materials that most effectively meet stringent requirements. Due to their adaptability, these materials may serve as versatile heat insulators and may be employed in a variety of high-temperature and corrosive surroundings.

Keywords

ракетный двигатель система скрепления теплозащитный экран абляция коксовый остаток

Received

29.09.2024

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GOST	Mironov V., Timarov A., Tolkach M. Thermal protection technologies for solid propellant rocket engines // Вестник Российской академии наук / Herald of the Russian Academy of Sciences. – 2024. – V. 94. – Issue number 7 C. 677-687 . URL: https://heraldras.ru/s0869587324070083-1/?version_id=105822. DOI: 10.31857/S0869587324070083
MLA	Mironov, V. V, Timarov, A. G, Tolkach, M. A "Thermal protection technologies for solid propellant rocket engines." Вестник Российской академии наук / Herald of the Russian Academy of Sciences. 94.7 (2024).:677-687. DOI: 10.31857/S0869587324070083
APA	Mironov V., Timarov A., Tolkach M. (2024). Thermal protection technologies for solid propellant rocket engines. Вестник Российской академии наук / Herald of the Russian Academy of Sciences. vol. 94, no. 7, pp.677-687 DOI: 10.31857/S0869587324070083

References

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