The hydrogenation
of metal nanoparticles provides a pathway
toward
tuning their combustion characteristics. Metal hydrides have been
employed as solid-fuel additives for rocket propellants, pyrotechnics,
and explosives. Gas generation during combustion is beneficial to
prevent aggregation and sintering of particles, enabling a more complete
fuel utilization. Here, we discuss a novel approach for the synthesis
of magnesium hydride nanoparticles based on a two-step aerosol process.
Mg particles are first nucleated and grown via thermal evaporation,
followed immediately by in-flight exposure to a hydrogen-rich low-temperature
plasma. During the second step, atomic hydrogen generated by the plasma
rapidly diffuses into the Mg lattice, forming particles with a significant
fraction of MgH2. We find that hydrogenated Mg nanoparticles
have an ignition temperature that is reduced by ∼200 °C
when combusted with potassium perchlorate as an oxidizer, compared
to the non-hydrogenated Mg material. This is due to the release of
hydrogen from the fuel, jumpstarting its combustion. In addition,
characterization of the plasma processes suggests that a careful balance
between the dissociation of molecular hydrogen and heating of the
nanoparticles must be achieved to avoid hydrogen desorption during
production and achieve a significant degree of hydrogenation.