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Experimental Characterization of a Composite Morphing Radiator Prototype in a Relevant Thermal Environment

机译:相关热环境下复合变形散热器原型的实验表征

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摘要

For future long duration space missions, crewed vehicles will require advanced thermal control systems to maintain a desired internal environment temperature in spite of a large range of internal and external heat loads. Current radiators are only able to achieve turndown ratios (i.e. the ratio between the radiator's maximum and minimum heat rejection rates) of approximately 3:1. Upcoming missions will require radiators capable of 12:1 turndown ratios. A radiator with the ability to alter shape could significantly increase turndown capacity. Shape memory alloys (SMAs) offer promising qualities for this endeavor, namely their temperature-dependent phase change and capacity for work. In 2015, the first ever morphing radiator prototype was constructed in which SMA actuators passively altered the radiator shape in response to a thermal load. This work describes a follow-on endeavor to demonstrate a similar concept using highly thermally conductive composite materials. Numerous versions of this new concept were tested in a thermal vacuum environment and successfully demonstrated morphing behavior and variable heat rejection, achieving a turndown ratio of 4.84:1. A summary of these thermal experiments and their results are provided herein.
机译:对于未来的长时间太空飞行任务,乘员车辆将需要先进的热控制系统,以维持所需的内部环境温度,尽管内部和外部的热负荷范围很大。当前的散热器只能实现大约3:1的调节比(即散热器最大散热率和最小散热率之比)。即将执行的任务将需要具有12:1调节比的散热器。具有改变形状能力的散热器可以显着提高调节能力。形状记忆合金(SMA)为这项工作提供了有前途的品质,即它们随温度变化的相变和工作能力。 2015年,建造了第一个变形散热器原型,其中SMA执行器根据热负载被动改变散热器的形状。这项工作描述了使用高导热复合材料来证明类似概念的后续工作。此新概念的许多版本都在热真空环境中进行了测试,并成功展示了变形行为和可变的散热性能,调节比为4.84:1。本文提供了这些热实验及其结果的摘要。

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