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Analysis Implementation, Verification, Validation and Performance of a Structurally-Integrated TPS Concept

机译:结构集成TPS概念的分析实施,验证,确认和性能

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This technical article describes the analysis implementation of a structurally-integrated thermal protection system (SITPS) concept in the HyperSizer structural sizing software. The software development is focused on integrating structural and thermal analysis methods for vehicle-level design of Highly Reliable Reusable Launch Systems (HRRLS) under the NASA Fundamental Aeronautics program. The unique feature of the SITPS concept is the AETB ceramic core which acts as an insulator between the hot outer surface and the cooler inner surface of the panel. The structural analysis is accomplished using panel homogenization. This results in an effective constitutive equation for the SITPS panel that is suitable for use in a full vehicle-scale finite element analysis. The thermal analysis of the SITPS concept is accomplished using an existing 1-D thermal analysis model that discretizes the structure and insulation into a series of thermal resistors and masses. Vehicle level sizing studies are included to compare the performance of SITPS to Gr/Ep and Al 2219 honeycomb sandwich concepts with traditional TPS shielding. These studies are used to establish accurate weight statements for a hypersonic SITPS vehicle concept. FEA verification is included in order to assess the accuracy of HyperSizer's eigenvalue predictions. Finally, the 1-D thermal analysis is validated by comparison of the results to published experimental data.
机译:本技术文章介绍了HyperSizer结构尺寸调整软件中结构集成式热保护系统(SITPS)概念的分析实现。该软件开发的重点是在NASA基础航空计划下,为高度可靠的可重复使用发射系统(HRRLS)的车辆级设计集成结构和热分析方法。 SITPS概念的独特之处在于AETB陶瓷芯,它充当面板的热外表面和较冷内表面之间的绝缘体。使用面板均质化完成结构分析。这为SITPS面板生成了一个有效的本构方程,适用于整个车辆规模的有限元分析。 SITPS概念的热分析是使用现有的一维热分析模型完成的,该模型将结构和绝缘离散为一系列热敏电阻和质量。包括车辆水平尺寸研究,以比较SITPS与具有传统TPS屏蔽的Gr / Ep和Al 2219蜂窝夹芯概念的性能。这些研究用于为超音速SITPS车辆概念建立准确的重量表述。包括FEA验证以评估HyperSizer特征值预测的准确性。最后,通过将结果与已发布的实验数据进行比较来验证一维热分析。

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