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Fizika Goreniya i Vzryva, 2023, Volume 59, Issue 5, Pages 22–32
DOI: https://doi.org/10.15372/FGV2022.9215 (Mi fgv1307) 		 
Analyzing the possibility of burning the launcher nose fairing elements

V. A. Arkhipova, A. A. Glazunova, N. N. Zolotorevab, E. A. Kozlova, A. G. Korotkikhac, V. T. Kuznetsova, V. I. Trushlyakovd

a Tomsk State University, Tomsk, Russia
b S.S. Kutateladze Institute of Thermophysics, Siberian Division of the Russian Academy of Sciences, Novosibirsk, Russia
c Tomsk Polytechnic University, Tomsk, Russia
d Omsk State Technical University, Omsk, Russia
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DOI: https://doi.org/10.15372/FGV2022.9215
Abstract: The results of an experimental study of the possibility of burning separated and discharged to the Earth's surface are presented on the example of the design of elements of the head fairing of a launch vehicle. A new scheme of a honeycomb-free three-layer construction of combusted elements of the head fairing using a charge of high-energy material is proposed. Based on the formulated requirements for the characteristics of the charge and analysis of the results of thermodynamic calculations, the basic compositions of high-energy materials (HEMs) were selected. The energy and strength characteristics of the selected HEM compositions are experimentally determined, and the patterns of their combustion at subatmospheric pressure are determined. The results of laboratory tests of the combustion of elements of the structures under consideration with a VEM filler charge showed the possibility of partial utilization of spent parts of the launch vehicle.
Keywords: space rocket, detachable nose fairing, combustion, high-energy materials, filler charge, organoplastic.
Funding agency Grant number
Program of Strategic Academic Leadership Prioritet-2030
Ministry of Science and Higher Education of the Russian Federation МК-2463.2022.4
Received: 03.08.2022
Revised: 06.10.2022
Accepted: 07.09.2022
English version:
Combustion, Explosion and Shock Waves, 2023, Volume 59, Issue 5, Pages 553–562
DOI: https://doi.org/10.1134/S0010508223050039
Bibliographic databases:
Document Type: Article
UDC: 662.221.11
Language: Russian
Citation: V. A. Arkhipov, A. A. Glazunov, N. N. Zolotorev, E. A. Kozlov, A. G. Korotkikh, V. T. Kuznetsov, V. I. Trushlyakov, “Analyzing the possibility of burning the launcher nose fairing elements”, Fizika Goreniya i Vzryva, 59:5 (2023), 22–32; Combustion, Explosion and Shock Waves, 59:5 (2023), 553–562
Citation in format AMSBIB
\Bibitem{ArkGlaZol23}
\by V.~A.~Arkhipov, A.~A.~Glazunov, N.~N.~Zolotorev, E.~A.~Kozlov, A.~G.~Korotkikh, V.~T.~Kuznetsov, V.~I.~Trushlyakov
\paper Analyzing the possibility of burning the launcher nose fairing elements
\jour Fizika Goreniya i Vzryva
\yr 2023
\vol 59
\issue 5
\pages 22--32
\mathnet{http://mi.mathnet.ru/fgv1307}
\crossref{https://doi.org/10.15372/FGV2022.9215}
\elib{https://elibrary.ru/item.asp?id=54484408}
\transl
\jour Combustion, Explosion and Shock Waves
\yr 2023
\vol 59
\issue 5
\pages 553--562
\crossref{https://doi.org/10.1134/S0010508223050039}
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