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REVIEW OF METHODS FOR DETERMINATION OF THERMAL EMISSIVITY

机译:测定热发射率测定方法

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摘要

Thermal emissivity is a key parameter for modelling of the thermal environment of spacecrafts. The ECSS-Q-70-09 describes methods for the determination of thermal emittance following different approaches: Thermal test method Infrared spectrometer Portable equipment. Due to the fundamental principles the methods are based on, not exactly the same parameter is determined, some methods cover the hemispherical emittance ε{sub}h (thermal infrared), others the normal emittance ε{sub}n (portable equipment). Whereas ε{sub}h is more representative for modelling, ε{sub}n is the more common parameter being determined. Taking the ECSS-Q-70-09 as a baseline, results obtained by the different approaches are shown to establish the reliability and the most common sources of error of each method.
机译:热发射率是用于造型的航天器热环境的键参数。 ECSS-Q-70-09描述了根据不同方法确定热发射的方法:热试验方法红外光谱仪便携式设备。由于该方法的基本原理基于,确定了不完全相同的参数,一些方法覆盖半球形发射ε{子} H(热红外),其他方法是正常发射ε{子} n(便携式设备)。 ε{sub} h更具模型的代表性,ε{sub} n是所确定的更常见的参数。将ECSS-Q-70-09作为基线,通过不同方法获得的结果显示为确保每种方法的可靠性和最常见的误差源。

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