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Updated: Mar 24, 2026

Laboratory Scale Slow Cook-Off Testing of Rocket Propellants: The Combustion Rate Analysis of a Slowly Heated Propellant CRASH-P Test
Published on: February 6, 2021
Tetrazole-based energetic coordination compounds as enhanced catalysts for the thermal decomposition of ammonium
Bo-Wen Fan1,2,3, Meng Cui2,3, Jing Qin4
1College of Chemistry and Materials Science, Fujian Normal University, Fuzhou, Fujian 350007, P. R. China.
Abstract:
Unlocking the potential of ammonium perchlorate (AP) by achieving a highly synergistic, rapid, and concentrated energy release process is essential for realizing a revolutionary improvement in the thrust of composite solid propellants. In this study, we employ a strategy that integrates a simple solution synthesis method with highly active Co2+ ions, tetrazole-based high-energy ligands, and high-energy ClO4- anions to prepare energetic coordination compounds (ECCs): [Co(1-MAT)6](ClO4)21 and [Co(2-MAT)4(H2O)2](ClO4)22. This approach achieves a dual enhancement by improving the catalytic performance of AP and significantly increasing the total heat release (ΔH) of the system. Single-crystal X-ray diffraction revealed that both compounds possess isolated structures, which was further supported by elemental analysis and FT-IR spectroscopy results. The high-temperature decomposition (HTD) of 1a (5 wt% of 1 in AP) exhibits excellent energy-release performance, as evidenced by a decrease in the exothermic peak temperature from 457 °C (pure AP) to 315 °C. Moreover, compared to pure AP (230 kJ mol-1, 559 J g-1), the mixture 1a showed a lowered activation energy of 144 kJ mol-1 along with a concomitant rise in ΔH to 1166 J g-1. In contrast to the baseline without additives, the addition of Al/AP to combustion pellet-based 1 and 2 resulted in a significant increase in the burning rate. This distinctive structure represents a good strategy designed to simultaneously enhance both the energy output and catalytic efficiency of propellants.
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