Analysis of the Hybrid Power System for High-Altitude Unmanned Aircraft

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Parameter</td><td align="center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">Wingspan</td><td align="center">22.5 m</td></tr><tr><td align="left">Chord</td><td align="center">1.185 m</td></tr><tr><td align="left">Area</td><td align="center">32.6 m<sup>2</sup></td></tr><tr><td align="left">Wing weight</td><td align="center">28 kg</td></tr><tr><td align="left">Aerofoil</td><td align="center">EPPLER 395</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Advances in Materials Science and Engineering

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Table 1

Table 1: Analysis of the Hybrid Power System for High-Altitude Unmanned Aircraft 