Experimental Study of Torque Using a Small Scoop on the Lunar Surface

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/8035456/figures/8035456.fig.007a.svgz" name="8035456.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Penetrating angle of 30°</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/8035456/figures/8035456.fig.007b.svgz" name="8035456.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Penetrating angle of 45°</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/8035456/figures/8035456.fig.007c.svgz" name="8035456.fig.007c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Penetrating angle of 60°</td></tr></table>

<div>Penetrating angle influence on the failure model. The soil condition was loose, no rocks were present, and the rotation speed was 0.28 r/min.</div>

International Journal of Aerospace Engineering

fig7

Figure 7

Figure 7: Experimental Study of Torque Using a Small Scoop on the Lunar Surface 