Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left"></td><td class="align_center">Max temp (°C)</td><td class="align_center">Min temp (°C)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Steady state</td><td class="align_center">+26 (+Y face)</td><td class="align_center">−38 (−Y face)</td></tr><tr><td class="align_left">Transient state</td><td class="align_center">+56 (+Y face)</td><td class="align_center">−35 (−Y face)</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

tab6

Table 6

Table 6: Design, Analysis, Optimization, Manufacturing, and Testing of a 2U Cubesat 