Research on the viscoelastic constitutive model of HTPB propellant over a wide range of strain rates

Hai Xia Zhou, Shi Peng Li, Kan Xie*, Xin Sui, Long Yang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

7 Citations (Scopus)

Abstract

To investigate the rate-dependent mechanical properties of hydroxyl-terminated polybutadiene (HTPB) propellant, low(1.67×10-4~1.67×10-1 s-1), intermediate(1~100 s-1), and high strain rate (700~2 500 s-1) compressive testing was performed, by using a universal testing machine, a hydraulic testing machine, and a split Hopkinson pressure bar (SHPB) system, respectively. Results indicate that the compressive mechanical properties of HTPB propellant are rate-dependent and the stress at a given strain increases with an increase in strain rate.Generalized nonlinear ZWT model was employed to describe the compressive mechanical behaviours of HTPB propellant over a wide range of strain rates.Compasrison of the predicted values from the model and the experimental data shows that the number of Maxwell elements in the model should be at least 4.

Original languageEnglish
Pages (from-to)325-329 and 396
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume40
Issue number3
DOIs
Publication statusPublished - 1 Jun 2017

Keywords

  • Compression
  • Constitutive model
  • HTPB propellant
  • Strain rate
  • Strain-rate correlation

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