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

The combustion chamber pressure had been calculated for four erosive burning models proposed by different authors. All the models showed convergence with the [...]

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

Key words: solid propellant charge mass , propellant combustion rate , combustion chamber pressure , operation time in starting and cruise modes , [...]

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9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

2016 (1); 59-62 Language: Russian Annotation: The purpose of work is development of simple and accurate procedure of calculation of scatter of SRM intraballistic parameters – [...]

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