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Emittance measurements of Space Shuttle orbiter reinforced carbon-carbon

机译:航天飞机轨道飞行器增强碳-碳的发射率测量

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摘要

The spectral and total normal emittance of the Reinforced Carbon-Carbon (RCC) used on Space Shuttle nose cap and wing leading edges has been measured at room temperature and at surface temperatures of 1200 to 2100 K. These measurements were made on virgin and two flown RCC samples. Room temperature directional emittance data were also obtained and were used to determine the total hemispherical emittance of RCC as a function of temperature. Results of the total normal emittance for the virgin samples showed good agreement with the current RCC emittance design curve; however, the data from the flown samples showed an increase in the emittance at high temperature possibly due to exposure from flight environments.
机译:已在室温和表面温度1200至2100 K下测量了航天飞机机头和机翼前缘上使用的增强碳-碳(RCC)的光谱和总法向发射率。这些测量是在原始和两次飞行时进行的RCC样本。还获得了室温方向的发射率数据,并将其用于确定RCC的总半球形发射率随温度的变化。原始样品的总正常发射率结果与当前的RCC发射率设计曲线吻合良好;然而,来自飞行样品的数据表明,高温下的发射率增加可能是由于暴露于飞行环境引起的。

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