Application of Honeycomb Structures in Key Components of Space Deployable Structures

<table class="table-group" id="tab3"><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">Maximum moment/mass</td><td class="align_center">Steady moment/mass</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Tape spring</td><td class="align_center">166.1408</td><td class="align_center">17.72121</td></tr><tr><td class="align_left">Model a</td><td class="align_center">259.0686</td><td class="align_center">18.57503</td></tr><tr><td class="align_left">Model b</td><td class="align_center">270.0811</td><td class="align_center">25.29373</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

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

Advances in Materials Science and Engineering

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Table 3

Table 3: Application of Honeycomb Structures in Key Components of Space Deployable Structures 