Application of Honeycomb Structures in Key Components of Space Deployable Structures

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left"> </td><td class="align_center">Mass (g)</td><td class="align_center">Maximum moment (Nmm)</td><td class="align_center">Steady moment (Nmm)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Tape spring</td><td class="align_center">53.625</td><td class="align_center">8909.3</td><td class="align_center">950.3</td></tr><tr><td class="align_left">Model a</td><td class="align_center">7.537</td><td class="align_center">1952.6</td><td class="align_center">140</td></tr><tr><td class="align_left">Model b</td><td class="align_center">12.086</td><td class="align_center">3264.2</td><td class="align_center">305.7</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison of mass, critical bending moment, and steady-state bending moment of different structures.</div>

Advances in Materials Science and Engineering

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Table 2

Table 2: Application of Honeycomb Structures in Key Components of Space Deployable Structures 