Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Altitude (km)</td><td class="align_center">Deorbiting velocity changes (m/s)</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">900</td><td class="align_center">204 (from 7400.5 to 7196.8)</td></tr><tr><td class="align_left">800</td><td class="align_center">178 (from 7451.5 to 7273.0)</td></tr><tr><td class="align_left">700</td><td class="align_center">153 (from 7504.3 to 7351.2)</td></tr><tr><td class="align_left">600</td><td class="align_center">127 (from 7557.9 to 7430.9)</td></tr><tr><td class="align_left">500</td><td class="align_center">101 (from 7612.6 to 7512.7)</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The required velocity changes in different altitudes.</div>

International Journal of Aerospace Engineering

tab2

Table 2

Table 2: Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit 