Analyzing the possibility of burning the launcher nose cone elements
| Parent link: | Combustion, Explosion and Shock Waves.— .— New York: Springer Science+Business Media LLC. Vol. 59, No. 5.— 2023.— P. 553-562 |
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| Corporate Author: | |
| Other Authors: | , , , , , , |
| Summary: | 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 |
| Language: | English |
| Published: |
2023
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| Subjects: | |
| Online Access: | https://doi.org/10.1134/S0010508223050039 |
| Format: | Electronic Book Chapter |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=672335 |
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| 200 | 1 | |a Analyzing the possibility of burning the launcher nose cone elements |f V. A. Arkhipov, A. A. Glazunov, N. N. Zolotorev [et al.] | |
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| 330 | |a 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 | ||
| 371 | 0 | |a AM_Agreement | |
| 461 | 1 | |t Combustion, Explosion and Shock Waves |c New York |n Springer Science+Business Media LLC. | |
| 463 | 1 | |t Vol. 59, No. 5 |v P. 553-562 |d 2023 | |
| 610 | 1 | |a электронный ресурс | |
| 610 | 1 | |a труды учёных ТПУ | |
| 610 | 1 | |a space-mission vehicle | |
| 610 | 1 | |a detachable nose cone | |
| 610 | 1 | |a combustion | |
| 610 | 1 | |a high-energy materials | |
| 610 | 1 | |a filler charge | |
| 610 | 1 | |a organoplastic | |
| 701 | 1 | |a Arkhipov |b V. A. |g Vladimir Afanasjevich | |
| 701 | 1 | |a Glazunov |b A. A. |g Anatoly Alekseevich | |
| 701 | 1 | |a Zolotorev |b N. N. |g Nikolay Nikolaevich | |
| 701 | 1 | |a Kozlov |b E. A. |g Evgeny Aleksandrovich | |
| 701 | 1 | |a Korotkikh |b A. G. |c specialist in the field of power engineering |c Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences |f 1976- |g Aleksandr Gennadievich |9 18113 | |
| 701 | 1 | |a Kuznetsov |b V. T. |g Valery Tikhonovich | |
| 701 | 1 | |a Trushlyakov |b V. I. |g Valery Ivanovich | |
| 712 | 0 | 2 | |a National Research Tomsk Polytechnic University |c (2009- ) |9 27197 |
| 801 | 0 | |a RU |b 63413507 |c 20240417 |g RCR | |
| 856 | 4 | |u https://doi.org/10.1134/S0010508223050039 |z https://doi.org/10.1134/S0010508223050039 | |
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