8.1.2024 Theoretic-experimental evaluation of the solid-propellant grain erosive burning

And in the process of propellant grain combustion, erosive burning often takes place (increase of propellant burning rate depending on combustion [...]

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10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM

The equations obtained show that the required parameters of diagrams (including consumption-thrust characteristics difference between the starting and cruise modes) can be ensured [...]

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20.1.2020 Studying the possibility of alternating delivery of rocket propellant wastes to a common thermal neutralization facility

The advantages of thermal neutralization units are considered, their operating principle is described, by the example of high-temperature toxic rocket propellants, the [...]

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2.1.2024 New and advanced liquid rocket engines of the Yuzhnoye SDO

2024, (1); 9-18 DOI: https://doi.org/10.33136/stma2024.01.009 Language: Ukrainian Annotation: Specialized design office for liquid engines was established on July 22, 1958 to [...]

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