Micromechanics equivalent modeling method for composite solid propellant

The invention discloses a composite solid propellant mesomechanics equivalent modeling method, and belongs to the technical field of spaceflight. The method specifically comprises the following steps: firstly, dividing oxidant particles in an actual formula of the composite solid propellant into sma...

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Bibliographic Details
Main Authors MAO CHENGLI, GAO HUANRAN, ZHANG JIANWEI, GENG WANGYANG
Format Patent
LanguageChinese
English
Published 03.11.2023
Subjects
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