Robust Design Optimization of an Aerospace Vehicle Prolusion System

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">Parameters</td><td align="center">Robust</td><td align="center">Optimal</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left"><span style="width: 37.75px;"><svg height="15.4" id="M163" style="vertical-align:-3.39069pt" version="1.1" viewbox="0 0 37.75 15.4" width="37.75" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg></span></td><td align="center">5.80</td><td align="center">6.11</td></tr><tr><td align="left"><svg height="15.4" id="M164" style="vertical-align:-3.3907pt" version="1.1" viewbox="0 0 12.2375 15.4" width="12.2375" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> (kN-sec)</td><td align="center">936.75</td><td align="center">965.55</td></tr><tr><td align="left"><svg height="14.875" id="M165" style="vertical-align:-5.73167pt" version="1.1" viewbox="0 0 21.2125 14.875" width="21.2125" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> (kg)</td><td align="center">404.10</td><td align="center">420.10</td></tr><tr><td align="left"><svg height="16.737499" id="M166" style="vertical-align:-4.4704pt" version="1.1" viewbox="0 0 49.625 16.737499" width="49.625" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> (MPa)</td><td align="center">14.55</td><td align="center">15.94</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

tab5

Table 5

Table 5: Robust Design Optimization of an Aerospace Vehicle Prolusion System 