МЕТОДИ ЕКСПЕРИМЕНТАЛЬНИХ ДОСЛІДЖЕНЬ ХАРАКТЕРИСТИК ТВЕРДОГО РАКЕТНОГО ПАЛИВА

DOI: https://doi.org/10.15407/itm2026.01.034 The process of designing a solid-propellant rocket engine is a complex problem. Usually, it is solved by an iterative method, in which the initial data are gradually refined using experimental studies. With a sufficient statistical database, the problem i...

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Bibliographic Details
Date:2026
Author Affiliations:
  • S. S. VASYLIV — https://orcid.org/ 0009-0000-0815-6323 Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine 15 Leshko-Popel St., Dnipro 49005, Ukraine; e-mail: gl_konstruktor@ukr.net
Keywords:keywords
Main Author: VASYLIV, S. S.
Format: Article
Language:Ukrainian
Published: текст 3 2026
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Online Access:https://journal-itm.dp.ua/ojs/index.php/ITM_j1/article/view/170
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Journal Title:Technical Mechanics
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Technical Mechanics

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