Development of a Novel Launch System Microwave Rocket Powered by Millimeter-Wave Discharge

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Frequency (wavelength)</td><td class="align_center">170 GHz (1.77 mm)</td></tr><tr><td class="align_left">Output power</td><td class="align_center">&gt;1 MW</td></tr><tr><td class="align_left">Output duration</td><td class="align_center">1 ms to 3600 s</td></tr><tr><td class="align_left">Beam transverse mode</td><td class="align_center">Gaussian</td></tr><tr><td class="align_left">Electric efficiency</td><td class="align_center">&gt;50%</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Characteristics of QST gyrotron [<a href="/journals/ijae/2018/9247429/#B16" target="_blank">16</a>].</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: Development of a Novel Launch System Microwave Rocket Powered by Millimeter-Wave Discharge 