Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster

<div>Test result of the hybrid thruster using neat H<sub>2</sub>O<sub>2</sub> and HDPE (P1 at feeding line, P2 at precombustor, P3 at postcombustor, and T1-3 at the catalyst bed upstream to downstream).</div>

International Journal of Aerospace Engineering

fig5

Figure 5

Figure 5: Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster 