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Constant Strain Aging Model of HTPB Propellant Involving Thermal–Mechanical Coupled Effects
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Constant Strain Aging Model of HTPB Propellant Involving Thermal–Mechanical Coupled Effects
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Journal Article
Constant Strain Aging Model of HTPB Propellant Involving Thermal–Mechanical Coupled Effects
2025
Overview
To investigate the aging behavior of HTPB composite solid propellant under constant strain conditions, this study analyzed the aging patterns of the propellant’s maximum elongation at four temperatures (323.15 K–343.15 K) and five strain levels (0–18%) using thermal–mechanical coupled accelerated aging tests. The results show that the maximum elongation initially increases, then decreases under constant strain conditions. To measure the mechanical work-induced decrease in the activation motor, we created a modified Arrhenius model with a strain correction factor based on empirical observations. The acceleration coefficient of a solid motor grain at the accelerated aging temperature (323.15 K) in comparison to the long-term storage temperature (293.15 K) was found to be 20.08 through finite element analysis. This means 206.80 days at the accelerated aging temperature is equivalent to 10 years at the long-term storage temperature.
