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Emission Spectroscopic Boundary Layer Investigation during Ablative Material Testing in Plasmatron

机译:等离子加速器烧蚀材料测试中的发射光谱边界层研究

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摘要

Ablative Thermal Protection Systems (TPS) allowed the first humans to safely return to Earth from the moon and are still considered as the only solution for future high-speed reentry missions. But despite the advancements made since Apollo, heat flux prediction remains an imperfect science and engineers resort to safety factors to determine the TPS thickness. This goes at the expense of embarked payload, hampering, for example, sample return missions. Ground testing in plasma wind-tunnels is currently the only affordable possibility for both material qualification and validation of material response codes. The subsonic 1.2MW Inductively Coupled Plasmatron facility at the von Karman Institute for Fluid Dynamics is able to reproduce a wide range of reentry environments. This protocol describes a procedure for the study of the gas/surface interaction on ablative materials in high enthalpy flows and presents sample results of a non-pyrolyzing, ablating carbon fiber precursor. With this publication, the authors envisage the definition of a standard procedure, facilitating comparison with other laboratories and contributing to ongoing efforts to improve heat shield reliability and reduce design uncertainties.The described core techniques are non-intrusive methods to track the material recession with a high-speed camera along with the chemistry in the reactive boundary layer, probed by emission spectroscopy. Although optical emission spectroscopy is limited to line-of-sight measurements and is further constrained to electronically excited atoms and molecules, its simplicity and broad applicability still make it the technique of choice for analysis of the reactive boundary layer. Recession of the ablating sample further requires that the distance of the measurement location with respect to the surface is known at all times during the experiment. Calibration of the optical system of the applied three spectrometers allowed quantitative comparison. At the fiber scale, results from a post-test microscopy analysis are presented.
机译:烧蚀热保护系统(TPS)使首批人类从月球安全返回地球,仍然被认为是未来高速重返飞行任务的唯一解决方案。但是,尽管自阿波罗(Apollo)以来取得了一些进步,但是热通量预测仍然是一门不完善的科学,工程师们还是依靠安全因素来确定TPS厚度。这是以装载有效载荷为代价的,例如妨碍了样品返回任务。目前,在等离子风洞中进行地面测试是材料鉴定和材料响应代码验证的唯一可承受的可能性。 von Karman流体动力学研究所的亚音速1.2MW感应耦合等离子装置能够重现各种折返环境。该协议描述了研究高焓流中烧蚀材料上气体/表面相互作用的程序,并给出了非热解烧蚀碳纤维前体的样品结果。在该出版物中,作者设想了标准程序的定义,以便于与其他实验室进行比较,并为提高隔热屏可靠性和减少设计不确定性做出的持续努力做出了贡献。高速相机以及反应性边界层中的化学物质,通过发射光谱进行探测。尽管光发射光谱法仅限于视线测量,并且进一步局限于电子激发的原子和分子,但其简单性和广泛的适用性仍使其成为反应性边界层分析的首选技术。消融样品的凹进还要求在实验过程中始终知道测量位置相对于表面的距离。所应用的三个光谱仪的光学系统的校准可以进行定量比较。在纤维规模上,显示了测试后显微镜分析的结果。

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