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- W1500508711 abstract "In solid rocket motors, a strong bond at the propellant–liner interface ensures that the propellant functions as designed. If the interface degums, the propellant burn surface area will change and the performance of internal ballistics will be adversely affected. In this study, two cases of motor failure are considered to investigate methods for improving the bond strength between the propellant grain and the liner interface, with the aim of achieving a tensile strength exceeding the 8 kg/cm2 requirement. Hydroxyl-terminated polybutadiene was used as the liner material. This hydroxyl-terminated-polybutadiene-based material was conditioned and processed under the conditions of 5–20 torr pressure and 60–70°C temperature. Further, toluene diisocyanate was considered as the hardener and its contents were increased in the liner by 0 (i.e., original content), 2, 5, 10, and 15% to obtain diisocyanate NCO/OH equivalence ratios of 1.035, 1.057, 1.087, 1.144, and 1.187, respectively. Thereafter, bond strength test..." @default.
- W1500508711 created "2016-06-24" @default.
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- W1500508711 date "2015-09-01" @default.
- W1500508711 modified "2023-09-23" @default.
- W1500508711 title "Improving Bond Strength at Propellant–Liner Interfaces" @default.
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- W1500508711 doi "https://doi.org/10.2514/1.b35700" @default.
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