Lightweight Photovoltaic Composite Structure on Stratospheric Airships

<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">Thickness of honeycomb core layer (mm)</td><td class="align_center">Increase of deflection (mm)</td><td class="align_center">Increase of structure weight (g)</td><td class="align_center">Deflection weight ratio (mm/(g/m<sup>2</sup>))</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">2</td><td class="align_center">5.6</td><td class="align_center">6.1</td><td class="align_center">0.0143</td></tr><tr><td class="align_left">5</td><td class="align_center">9.4</td><td class="align_center">7.97</td><td class="align_center">0.0184</td></tr><tr><td class="align_left">8</td><td class="align_center">4.5</td><td class="align_center">9.4</td><td class="align_center">0.0075</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Deflection weight ratio with different thicknesses.</div>

Advances in Materials Science and Engineering

tab5

Table 5

Table 5: Lightweight Photovoltaic Composite Structure on Stratospheric Airships 