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

<div>MnO<sub>x</sub>/Al<sub>2</sub>O<sub>3</sub> catalyst after the firing test using neat (a) and gel (b) H<sub>2</sub>O<sub>2</sub>.</div>

International Journal of Aerospace Engineering

Figure 7: Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster 