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

<table class="table-group" id="tab17"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><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">Tensile strength (MPa)</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Carbon fiber T700</td><td class="align_center">1800</td><td class="align_center">126</td><td class="align_center">0.31</td><td class="align_center">3500</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Material parameters of the deployment mechanism.</div>

International Journal of Aerospace Engineering

tab17

Table 17

Table 17: Method for Predicting the Liquid-Sloshing Characteristics of a Microsatellite Propulsion System 