The Eu:CROPIS Mass Property Campaign: Trimming a Spin-Stabilized Compact Satellite for a Long-Term Artificial Gravity Experiment

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Satellite configuration</td><td class="align_center">Separation system</td><td class="align_center">Solar panels</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Launch configuration</td><td class="align_center">Launch configuration</td><td class="align_center">Stowed</td></tr><tr><td class="align_left">Stowed configuration</td><td class="align_center">Flight configuration</td><td class="align_center">Stowed</td></tr><tr><td class="align_left">Deployed configuration</td><td class="align_center">Flight configuration</td><td class="align_center">Deployed</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Nominal configuration statuses.</div>

International Journal of Aerospace Engineering

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Table 1

Table 1: The Eu:CROPIS Mass Property Campaign: Trimming a Spin-Stabilized Compact Satellite for a Long-Term Artificial Gravity Experiment 