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

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Temperature difference (<span class="nowrap"><svg height="11.0292pt" id="M28" style="vertical-align:-0.2325001pt" version="1.1" viewbox="-0.0498162 -10.7967 12.7918 11.0292" width="12.7918pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.0091,0,0,-0.0091,0,-5.741)"><path d="M339 262C339 340 273 403 193 403S48 340 48 262S113 121 193 121S339 184 339 262ZM283 262C283 210 242 168 193 168S104 210 104 262S144 356 193 356S283 314 283 262Z"></path></g><g transform="matrix(.013,0,0,-0.013,4.015,0)"><path d="M614 175C564 76 510 21 408 21C256 21 146 149 146 336C146 488 235 629 402 629C510 629 570 586 597 480L626 488C620 541 614 582 606 638C578 643 510 665 429 665C206 665 44 527 44 316C44 157 153 -15 402 -15C474 -15 558 5 586 11C604 45 629 119 643 165L614 175Z"></path></g></svg>)</span></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">7.76</td><td class="align_center">63.72</td><td class="align_center">260.4</td><td class="align_center">45</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 honeycomb aluminum plate.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Performance Optimization and Verification of a New Type of Solar Panel for Microsatellites 