Study on Heat Exchange Structure Design and Propulsion Performance of Solar Thermal Thruster

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/1348289/figures/1348289.fig.0011a.svgz" name="1348289.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Comparison of 3D simulation and 1D simulation results when the mass flow rate was <svg height="14.9947pt" id="M124" style="vertical-align:-3.4033pt" version="1.1" viewbox="-0.0498162 -11.5914 83.3089 14.9947" width="83.3089pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M384 0V27C293 34 287 42 287 114V635C232 613 172 594 109 583V559L157 557C201 555 205 550 205 499V114C205 42 199 34 109 27V0H384Z"></path></g><g transform="matrix(.013,0,0,-0.013,6.24,0)"><path d="M113 -12C146 -12 170 11 170 46C170 78 146 103 114 103S58 78 58 46C58 11 82 -12 113 -12Z"></path></g><g transform="matrix(.013,0,0,-0.013,9.204,0)"><path d="M384 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<div>Comparison of 3D simulation and 1D simulation results under different mass flow rates.</div>

International Journal of Aerospace Engineering

fig11

Figure 11

Figure 11: Study on Heat Exchange Structure Design and Propulsion Performance of Solar Thermal Thruster 