Method for Predicting the Liquid-Sloshing Characteristics of a Microsatellite Propulsion System

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr class="thead"><td class="align_left">Material</td><td class="align_center">Density (kg/m<sup>3</sup>)</td><td class="align_center">Modulus of elasticity (GPa)</td><td class="align_center">Poisson ratio</td><td class="align_center">Yield strength (MPa)</td><td class="align_center">Tensile strength (MPa)</td></tr><tr><td class="thead-hr" colspan="6"><hr/></td></tr><tr><td class="align_left">TC4</td><td class="align_center">4500</td><td class="align_center">120</td><td class="align_center">0.3</td><td class="align_center">850</td><td class="align_center">1100</td></tr><tr class="table-tr"><td colspan="6"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The material properties for the storage tank.</div>

International Journal of Aerospace Engineering

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Table 2

Table 2: Method for Predicting the Liquid-Sloshing Characteristics of a Microsatellite Propulsion System 