A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage

<div>Step-by-step equivalent RVE model of a four-component HTPB propellant (unit: <i>μ</i>m). (a) Contains small-sized particles. (b) Contains large-sized particles.</div>

International Journal of Aerospace Engineering

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Figure 2

Figure 2: A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage 