热电偶
材料科学
热的
温度测量
机械工程
复合材料
工程类
气象学
物理
量子力学
作者
Colin M. Yee,Matt Ray,Felix Tang,Jonathan Wan,Richard Tatuaca,Maurizio Natali,Joseph H. Koo
出处
期刊:Journal of Spacecraft and Rockets
[American Institute of Aeronautics and Astronautics]
日期:2014-09-18
卷期号:51 (6): 1789-1796
被引量:15
摘要
This study involved the development of an in situ ablation sensor designed to evaluate the recession rate for an ablative thermal protection system exposed to a hyperthermal environment. Design requirements specify that the sensor be constructed using multiple thermocouples at staggered depths, drilled and mounted into carbon/carbon composite and carbon/phenolic ablatives. During erosion, the thermocouples record thermal data and then melt when the flame front approaches the thermocouples. The position of the recession front and breaking time of the thermocouple can determine the ablation rate. Earlier designs developed by the authors’ research group involved the use of 0.25-mm-diam thermocouples and electric discharge machining. Later designs used 0.5-mm-diam thermocouples using conventional microdrilling: This approach can be used in all applications in which the intrusiveness of the thermocouple embedded in the thermal protection system is not a primary requirement and allows 0.5 mm thermocouples to be used as a replacement for ultrasmall and costly 0.25 mm thermocouples.
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