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KINETICS OF THERMAL DEGRADATION OF THERMOPLASTIC POLYURETHANE ELASTOMER NANOCOMPOSITES

机译:热塑性聚氨酯弹性体纳米复合材料热降解的动力学

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Thermal protection materials are required to protect structural components of space vehicles during the re-entry stage, missile launching systems, and solid rocket motors. Novel materials based on nanotechnology creating nontraditional ablators are rapidly changing the technology base for thermal protection systems. The introduction of inorganic nanomaterials as additives into polymer systems has resulted in polymer nanostructured materials exhibiting multifunctional, high-performance polymer characteristics beyond traditional polymer composites possess. In this study, different polymer nanocomposite compositions were created by melt-compounded montmorillonite nanoclays or carbon nanofibers in a neat thermoplastic polyurethane elastomer (TPU) polymer using twin-screw extrusion. Selective materials were characterized for their thermal and kinetic properties. Results were then compared against the current state-of-the-art insulation material, Kevlar~R-filled ethylene-propylene-diene rubber (EPDM) as well as the neat TPU for the investigation of kinetic parameters.
机译:在重新进入阶段,导弹发射系统和固体火箭电动机期间,需要热保护材料来保护太空车辆的结构部件。基于纳米技术的新型材料创建非传统消耗器正在快速改变热保护系统的技术基础。作为添加剂进入聚合物体系的无机纳米材料的引入导致聚合物纳米结构材料表现出超出传统聚合物复合材料的多功能高性能聚合物特性。在该研究中,使用双螺杆挤出,通过熔融配混的蒙脱石纳米酰纳米粘土或碳纳米纤维产生不同的聚合物纳米复合材料组合物。使用双螺杆挤出,通过纯热塑性聚氨酯弹性体(TPU)聚合物中的碳纳米纤维产生。选择性材料的特征是其热和动力学性质。然后将结果与目前的最先进的绝缘材料,Kevlar〜R填充乙烯 - 丙烯 - 二烯橡胶(EPDM)以及纯TPU进行比较,用于研究动力学参数。

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