Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/6439787/figures/6439787.fig.003a.svgz" name="6439787.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Curves of TG-DTG for NEPE propellant</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/6439787/figures/6439787.fig.003b.svgz" name="6439787.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Curves of DSC for NEPE propellant</td></tr></table>

<div>TG-DTG and DSC curves for NEPE propellant.</div>

International Journal of Aerospace Engineering

fig3

Figure 3

Figure 3: Thermal Decomposition, Ignition Process and Combustion Behavior of Nitrate Ester Plasticized Polyether Propellant at 0.1–3.0 MPa 