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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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
03.11.2023
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Subjects | |
Online Access | Get full text |
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