Abstract

A comparative thermal decomposition kinetic investigation on Fe(III) complexes of a antipyrine Schiff base ligand, 1,2-Bis(imino-4’-antipyrinyl)ethane (GA)), with varying counter anions viz. CIO4-, NO3-, SCN-, Cl-, and Br-, has been done by thermogravimetric analysis by using Coats-Redfern equation. The kinetic parameters like activation energy (E), pre-exponential factor (A) and entropy of activation (ΔS) were quantified. On comparing the various kinetic parameters, lower activation energy was observed in second stage as compared to first thermal decomposition stage. The same trend has been observed for pre-exponential factor (A) and entropy of activation (ΔS). The present results show that the starting materials having higher activation energy (E), are more stable than the intermediate products, however; the intermediate products possess well-ordered chemical structure due to their highly negative entropy of activation (ΔS) values. The present investigation proves that the counter anions play an important role on the thermal decomposition kinetics of the complexes.

Highlights

  • Elemo et al DOIThermal decomposition kinetics analysis of solid propellants can be correlated to combustion characteristics of the fuels [3]

  • On comparing the various kinetic parameters, lower activation energy was observed in second stage as compared to first thermal decomposition stage

  • The present investigation proves that the counter anions play an important role on the thermal decomposition kinetics of the complexes

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Summary

Elemo et al DOI

Thermal decomposition kinetics analysis of solid propellants can be correlated to combustion characteristics of the fuels [3]. We have thermally characterised five Fe(III) coordination complexes, which has been synthesised and characterised by the reported procedure [7], and their thermal decomposition kinetics, based on various kinetic parameters like activation energy (E), entropy activation (∆S), pre-exponential factor (A), are evaluated by Coats-Redfern equation. This kinetic evaluation can be used as photo type for energetic characteristics of solid propellants

Experimental
Results and Discussion
Principle
Phenomenological Aspects
Kinetic Aspects
Comparison of the Kinetic Parameters with Structure and Thermal Stability
Conclusion and Summary

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