Analyzing the possibility of burning the launcher nose cone elements

Analyzing the possibility of burning the launcher nose cone elements

Dades bibliogràfiques
Parent link:Combustion, Explosion and Shock Waves.— .— New York: Springer Science+Business Media LLC.
Vol. 59, No. 5.— 2023.— P. 553-562
Autor corporatiu: National Research Tomsk Polytechnic University
Altres autors: Arkhipov V. A. Vladimir Afanasjevich, Glazunov A. A. Anatoly Alekseevich, Zolotorev N. N. Nikolay Nikolaevich, Kozlov E. A. Evgeny Aleksandrovich, Korotkikh A. G. Aleksandr Gennadievich, Kuznetsov V. T. Valery Tikhonovich, Trushlyakov V. I. Valery Ivanovich
Sumari:Title screen
This paper describes an experimental study of the possibility of combustion of launcher nose cone elements separated and discharged to the Earth’s surface. A new schematic diagram of a honeycomb-free three-layer structure of the nose cone elements burned using a high-energy material charge is proposed. Based on the requirements formulated for the charge characteristics and the analysis of thermodynamic calculations, the base compositions of the high-energy materials are selected. The energy and strength characteristics of the selected HEM compositions are experimentally determined, and their combustion patterns at subatmospheric pressure are determined. It is shown by the laboratory tests on the combustion of the structural elements under consideration with a HEM filler charge that the spent parts of the launcher can be partially utilized
AM_Agreement
Idioma:anglès
Publicat: 2023
Matèries:
электронный ресурс
труды учёных ТПУ
space-mission vehicle
detachable nose cone
combustion
high-energy materials
filler charge
organoplastic
Accés en línia:https://doi.org/10.1134/S0010508223050039
Format: Electrònic Capítol de llibre
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=672335

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