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

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Year</td><td class="align_center">2009</td><td class="align_center">2011</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Beam power @pulse repetition frequency</td><td class="align_center">270 kW @ 50 Hz</td><td class="align_center">570 kW @ 200 Hz</td></tr><tr><td class="align_left"><i>C</i><sub>m</sub></td><td class="align_center">100 N/MW</td><td class="align_center">360 N/MW</td></tr><tr><td class="align_left">Time averaged thrust</td><td class="align_center">2.3 N</td><td class="align_center">30 N</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Thrust performance and operation conditions [<a href="/journals/ijae/2018/9247429/#B23" target="_blank">23</a>].</div>

International Journal of Aerospace Engineering

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Table 2: Development of a Novel Launch System Microwave Rocket Powered by Millimeter-Wave Discharge 