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Repeatability Measurements of Apparent Thermal Conductivity of Multilayer Insulation (MLI)

机译:多层绝缘表观导热率的可重复性测量(MLI)

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This report presents and discusses the results of repeatability experiments gathered from the multi-layer insulation thermal conductivity experiment (MIKE) for the measurement of the apparent thermal conductivity of multi-layer insulation (MLI) at variable boundary temperatures. Our apparatus uses a calibrated thermal link between the lower temperature shield of a concentric cylinder insulation assembly and the cold head of a cryocooler to measure the heat leak. In addition, thermocouple readings are taken in-between the MLI layers. These measurements are part of a multi-phase NASA-Yetispace-FSU collaboration to better understand the repeatability of thermal conductivity measurements of MLI. NASA provided five 25 layer coupons and requested boundary temperatures of 20 K and 300 K. Yetispace provided ten 12-layer coupons and requested boundary temperatures of 77 K and 293 K. Test conditions must be met for a duration of four hours at a steady state variance of less than 0.1 K/hr on both cylinders. Temperatures from three Cernox~R temperature sensors on each of the two cylinders are averaged to determine the boundary temperatures. A high vacuum, less than 10~(-5) torr, is maintained for the duration of testing. Layer density varied from 17.98 - 26.36 layers/cm for Yetispace coupons and 13.05 - 17.45 layers/cm for the NASA coupons. The average measured heat load for the Yetispace coupons was 2.40 W for phase-one and 2.92 W for phase-two. The average measured heat load for the NASA coupons was 1.10 W. This suggests there is still unknown variance of MLI performance. It has been concluded, variations in the insulation installation heavy effect the apparent thermal conductivity and are not solely dependent on layer density.
机译:此报告呈现并讨论的从多层绝缘的热导率实验(MIKE)聚集在变边界温度多层绝缘(MLI)的表观导热率的测量重复性实验的结果。我们的装置使用同心圆筒绝缘组件的下部温度屏蔽和低温冷却器来测量热泄漏的冷头之间的校准的热链接。此外,热电偶读数时在其之间的MLI层。这些测量以更好地理解MLI的热导率测量的可重复性的多相NASA-Yetispace-FSU协作的一部分。 20 K和300 K. Yetispace的NASA设置五个25层的优惠券和请求的边界温度设置10 12层的优惠券和要求77 K和293个K.试验条件的边界的温度必须在稳定状态满足的四个小时的持续时间在两个气缸小于0.1的K / hr的方差。从在每一个的两个气缸三个Cernox〜 - [R温度传感器的温度进行平均,以确定边界温度。的高真空,小于10〜(-5)托,保持用于测试的持续时间。层密度为17.98变化 - 26.36层/厘米Yetispace优惠券和13.05 - 17.45层/厘米为NASA的优惠券。用于Yetispace试样测得的平均热负荷为2.40 W代表相酮和2.92 W代表相两。为NASA的优惠券的平均测得的热负荷为1.10 W.这表明仍有的MLI性能未知方差。已经结束,在绝缘安装重效应的变化的表观导热率,并且不仅取决于层的密度。

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