Performance Optimization and Verification of a New Type of Solar Panel for Microsatellites

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Temperature difference (°C)</td><td class="align_center">Compression strength (MPa)</td><td class="align_center">Shear strength (MPa)</td><td class="align_center">Weight (g)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">0.63</td><td class="align_center">61.32</td><td class="align_center">209.4</td><td class="align_center">67.2</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Performance analysis results of the new type of solar panel.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Performance Optimization and Verification of a New Type of Solar Panel for Microsatellites 