Abstract
Aluminum hydride (AlH3) exhibits attractive properties, such as high hydrogen/energy storage, relatively good stability, and low dehydrogenation temperature. Thus, AlH3 has appreciable prospects as a component in solid propellant for promoting the specific impulse of rocket engines and for effectively reducing the erosion of engine nozzles. The TG-MS, SEM, XRD, XPS, and EDS results show that the thermal reaction of AlH3 is divided into three stages: (1) Dehydrogenation (below 210 °C, 2AlH3→2Al+3H2) starts from the inherent defects on the surface with an incomplete decomposition due to the passivation reaction in which an amorphous Al2O3 layer is formed to encapsulate the contained hydrogen. This is accompanied by nucleation and growth of Al nuclei from the outer particles to the inner particles and the formation of H2O via oxidation of the generated hydrogen. (2) The primary oxidation of Al (210–650 °C, 4Al+3O2→2γ-Al2O3) is attributed to a discontinuous layer of γ-Al2O3, which is transformed from amorphous Al2O3 that results in the reaction of naked residual Al and O2. (3) The secondary oxidation of residual Al (above 650 °C, 4Al+3O2→2α-Al2O3) occurs because of the crystal conversion from γ-Al2O3 to α-Al2O3, which leads to the shrinkage of the oxide shell and to the formation of cracks. Also, melting of residual Al breaks the shell, and this induces further oxidation. The results obtained for the microscopic kinetics mechanisms of dehydrogenation and oxidation of AlH3, show a clear direction for research regarding modifications of AlH3 as the theoretical foundation and are beneficial for the wide use of AlH3 in applications such as solid propellant as an energetic material and as a hydrogen source for fuel cells.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have