Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1015674/figures/1015674.fig.009a.svgz" name="1015674.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Impact angle is 72°</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1015674/figures/1015674.fig.009b.svgz" name="1015674.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Impact angle is 70°</td></tr></table>

<div>Critical penetration of the rear face sheet.</div>

International Journal of Aerospace Engineering

fig9

Figure 9

Figure 9: Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure 