Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/2700740/figures/2700740.fig.006a.svgz" name="2700740.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Original aging development equations of VPR</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/2700740/figures/2700740.fig.006b.svgz" name="2700740.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Modified aging development equations of VPR</td></tr></table>

<div>VPR under different aging times and its fitting curves.</div>

International Journal of Aerospace Engineering

fig6

Figure 6

Figure 6: Investigation on Aging Model of Solid Propellant Using the Degree of Crosslinking 