Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="649753.fig.005a" src="https://static.hindawi.com/articles/ijae/volume-2012/649753/figures/649753.fig.005a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Triangular-port geometry</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="649753.fig.005b" src="https://static.hindawi.com/articles/ijae/volume-2012/649753/figures/649753.fig.005b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Quadrilateral-port geometry</td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

fig5

Figure 5

Figure 5: Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines 