Research on Tensile Stress–Strain Relationship of Azide Polyether Propellant for Wide‐Temperature Range Based on Time–Temperature Superposition Principle

ABSTRACT Azide polyether propellants are emerging high‐energy solid propellants and have broad application prospects. To determine their mechanical properties under wide temperature ranges, tensile tests were conducted considering different combinations of temperature and loading rate, and the corresponding tensile stress–strain curves were plotted. The influence laws of temperature and loading rate on the materials' tensile response were revealed through qualitative and quantitative analyses. The applicability of the time–temperature superposition principle to the nonlinear deformation stage of the propellant was proved, and a stress response prediction method derived from this principle that solely relies on dynamic mechanical analysis and tensile test data was established.

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Publication Details

Journal
Propellants Explosives Pyrotechnics
Published
2024-12-07
DOI
https://doi.org/10.1002/prep.202400145
Citations
3
Primary Topic
Energetic Materials and Combustion
Type
article
Field-Weighted Citation Impact
0.81
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article

Research on Tensile Stress–Strain Relationship of Azide Polyether Propellant for Wide‐Temperature Range Based on Time–Temperature Superposition Principle

Xiuduo Song, Weilu Yang, Zhifeng Yuan, Yiwen Hu et al.
3 citations
Propellants Explosives Pyrotechnics
Energetic Materials and Combustion
0.81
article

Research on Tensile Stress–Strain Relationship of Azide Polyether Propellant for Wide‐Temperature Range Based on Time–Temperature Superposition Principle

Xiuduo Song, Weilu Yang, Zhifeng Yuan, Yiwen Hu, Gang Wang
article en
3 citations

Abstract

ABSTRACT Azide polyether propellants are emerging high‐energy solid propellants and have broad application prospects. To determine their mechanical properties under wide temperature ranges, tensile tests were conducted considering different combinations of temperature and loading rate, and the corresponding tensile stress–strain curves were plotted. The influence laws of temperature and loading rate on the materials' tensile response were revealed through qualitative and quantitative analyses. The applicability of the time–temperature superposition principle to the nonlinear deformation stage of the propellant was proved, and a stress response prediction method derived from this principle that solely relies on dynamic mechanical analysis and tensile test data was established.

Propellants Explosives PyrotechnicsVol. 50(2)
Modern Electron (United States) (US)
Openalex Percentile: Top 31%
Energetic Materials and Combustion
0.81
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