Distinctive experimental approach to provide the framework for designing H2O2 injector. Showerhead injector and impinging jet injector were considered. Manganese oxide/γ-alumina and manganese oxide/lanthanum doped alumina were utilized. Clarifying that showerhead injector is favorable for H2O2 monopropellant thruster Clarifying that impinging jet injector is beneficial to bipropellant engine using H2O2 decomposition