Abstract

Ammonium perchlorate (AP) is the universal oxidiser in use for all the solid rocket propellant motors used for space exploration due to its high available oxygen content and thermal decomposition without any solid residue. The inclusion of reactive species in AP directly affect the viscoelastic and ballistic properties of the propellant. Variations in lattice configuration of AP change its physical and thermal characteristics dramatically. In the present work AP was doped with Copper perchlorate and Iron perchlorate through co crystallisation. The impact of inclusion of these ionic species in the lattice on the thermal decomposition characteristics of AP was examined. The incorporation affected the physical as well as the ballistic characteristics of the resultant AP. The incorporation of foreign ions into AP crystals significantly changed the crystal morphology. The decomposition temperature decreased vis-a-vis with normal AP. The activation energy remarkably decreased for the doped AP crystals.

Highlights

  • The important chemical formulation used in rocketry is Composite Solid Propellant (CSP)

  • The specific surface area of normal and doped Ammonium perchlorate (AP) crystals were measured using multipoint BET and it is in the range 0.17–0.19 m2/g for normal AP and 0.22–0.24 m2/g for copper/iron doped AP

  • The decomposition characteristics of AP crystals were improved by lattice modification with iron perchlorate and copper perchlorate

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Summary

Introduction

The important chemical formulation used in rocketry is Composite Solid Propellant (CSP). Impact of lattice inclusion of Cu and Fe ions on thermal decomposition characteristics of ammonium perchlorate. The doped AP crystals were analysed for studying the impact of lattice inclusion of Cu and Fe ions on the lattice, physical and thermal characteristics of AP.

Results
Conclusion
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