Design of the Space Camera Protection System during Launch Process

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Modal order</td><td class="align_center">Frequency</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">24.2 Hz</td></tr><tr><td class="align_left">2</td><td class="align_center">25.1 Hz</td></tr><tr><td class="align_left">3</td><td class="align_center">45.5 Hz</td></tr><tr><td class="align_left">4</td><td class="align_center">48.0 Hz</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Calculation results of the first 4 modes.</div>

International Journal of Aerospace Engineering

tab3

Table 3

Table 3: Design of the Space Camera Protection System during Launch Process 