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New method for evaluating the kinetic constant of thermal protection materials

机译:评价热防护材料动力学常数的新方法

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Thermal protection material (TPM) is used to protect rocket structures from extreme conditions created by the hot exhaust of the rocket. Designing TPM is an important step in the rocket design process. Considering that an increase in the system weight decreases the overall performance of a rocket, the amount of TPM is carefully determined during the design process. Therefore, the precise properties of TPM guarantee an accurate thermal analysis and the successful design of the rocket. Among the many properties of TPM, the kinetic constant and activation energy, which govern the thermochemical reaction of the TPM, are the most important. Thus, an experiment to measure the kinetic constant and activation energy is conducted as part of this research. A theoretical approach to deduce the properties from measured data is discussed, and a method to apply the theory to experimental data, termed the R2 method, is developed. Compared to a previous method which was difficult to apply, the R2 method reduces unclear selections of the reaction time and does not require intervention by an interpreter. The properties deduced by the R2 method show good agreement with the other method despite the limited number of experimental results.
机译:热保护材料(TPM)用于保护火箭结构免受火箭高温排气所产生的极端条件的影响。 TPM的设计是火箭设计过程中的重要一步。考虑到系统重量的增加会降低火箭的整体性能,因此在设计过程中会仔细确定TPM的数量。因此,TPM的精确特性保证了精确的热分析和火箭的成功设计。在TPM的许多特性中,控制TPM的热化学反应的动力学常数和活化能最为重要。因此,作为该研究的一部分,进行了测量动力学常数和活化能的实验。讨论了一种从测量数据推导特性的理论方法,并开发了一种将该理论应用于实验数据的方法,称为R2方法。与以前难以应用的方法相比,R2方法减少了对反应时间的不清楚选择,并且不需要翻译人员的干预。尽管实验结果数量有限,但通过R2方法推导的性能与另一种方法显示出良好的一致性。

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