Effect of neutral polymeric bonding agent on tensile mechanical properties and damage evolution of NEPE propellant

M. Wubuliaisan, Yanqing Wu*, Xiao Hou, Kun Yang, Hongzheng Duan, Xinmei Yin

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

5 Citations (Scopus)

Abstract

Introducing Neutral Polymeric bonding agents (NPBA) into the Nitrate Ester Plasticized Polyether (NEPE) propellant could improve the adhesion between filler/matrix interface, thereby contributing to the development of new generations of the NEPE propellant with better mechanical properties. Therefore, understanding the effects of NPBA on the deformation and damage evolution of the NEPE propellant is fundamental to material design and applications. This paper studies the uniaxial tensile and stress relaxation responses of the NEPE propellant with different amounts of NPBA. The damage evolution in terms of interface debonding is further investigated using a cohesive-zone model (CZM). Experimental results show that the initial modulus and strength of the NEPE propellant increase with the increasing amount of NPBA while the elongation decreases. Meanwhile, the relaxation rate slows down and a higher long-term equilibrium modulus is reached. Experimental and numerical analyses indicate that interface debonding and crack propagation along filler–matrix interface are the dominant damage mechanism for the samples with a low amount of NPBA, while damage localization and crack advancement through the matrix are predominant for the ones with a high amount of NPBA. Finally, crosslinking density tests and simulation results also show that the effect of the bonding agent is interfacial rather than due to the overall crosslinking density change of the binder.

Original languageEnglish
Pages (from-to)357-367
Number of pages11
JournalDefence Technology
Volume32
DOIs
Publication statusPublished - Feb 2024

Keywords

  • Bonding agent
  • Cohesive-zone model
  • Damage evolution
  • Interface debonding
  • Mechanical properties
  • Solid propellant

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