What could be the best chemical catalyst diluted in a fuel to use in a liquid rocket motor for 90% of H2O2? The idea is to avoid a big catalytic reactor before the combustion chamber of the rocket motor and to provide decomposition directly inside the combustion chamber.

There could be CuCl2 as an option, but its concentration should be around 10% of hydrogen peroxide by mass which doesn't make it feasible for rocket applications.

Are there any publications in this area indicating possible species and concentrations of H2O2 chemical catalysts?

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