Analyzing the Possibility of Burning the Launcher Nose Cone Elements

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 propos...

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Bibliographic Details
Published in:Combustion, explosion, and shock waves explosion, and shock waves, 2023-10, Vol.59 (5), p.553-562
Main Authors: Arkhipov, V. A., Glazunov, A. A., Zolotorev, N. N., Kozlov, E. A., Korotkikh, A. G., Kuznetsov, V. T., Trushlyakov, V. I.
Format: Article
Language:English
Subjects:
Charge materials
Classical and Continuum Physics
Classical Mechanics
Combustion
Composition
Control
Dynamical Systems
Earth surface
Engineering
Laboratory tests
Launchers
Nose cones
Physical Chemistry
Physics
Physics and Astronomy
Structural members
Vibration
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Summary: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.
ISSN:0010-5082
1573-8345
DOI:10.1134/S0010508223050039