Vibration and Modal Analysis of Low Earth Orbit Satellite

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left"> </td><td align="center">Normal to the mounting plane</td><td align="center">Parallel to the mounting plane</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">Freq. <svg height="14.85" id="M31" style="vertical-align:-1.95624pt" version="1.1" viewbox="0 0 5.9875002 14.85" width="5.9875002" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.062,12.012)"><path d="M290 -163h-170v866h170v-28q-79 -7 -94 -19.5t-15 -72.5v-627q0 -59 14.5 -71.5t94.5 -19.5v-28z" id="x5B"></path></g>
</svg>Hz<svg height="14.85" id="M32" style="vertical-align:-1.95624pt" version="1.1" viewbox="0 0 5.9875002 14.85" width="5.9875002" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.062,12.012)"><path d="M226 -163h-170v27q79 7 94 20t15 73v627q0 59 -15 72t-94 20v27h170v-866z" id="x5D"></path></g>
</svg></td><td align="center" colspan="2">Levels</td></tr><tr><td align="left">0–200</td><td align="center">12 g</td><td align="center">8 g</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Shock and Vibration

tab2

Table 2

Table 2: Vibration and Modal Analysis of Low Earth Orbit Satellite 