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Evaporative Heat Transfer Mechanisms within a Heat Melt Compactor

机译:热熔压实机内的蒸发传热机理

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This paper will discuss the status of microgravity analysis and testing for the development of a Heat Melt Compactor (HMC). Since fluids behave completely differently in microgravity, the evaporation process for the HMC is expected to be different than in 1-g. A thermal model is developed to support the design and operation of the HMC. Also, low-gravity aircraft flight data is described to assess the point at which water may be squeezed out of the HMC during microgravity operation. For optimum heat transfer operation of the HMC, the compaction process should stop prior to any water exiting the HMC, but nevertheless seek to compact as much as possible to cause high heat transfer and therefore shorter evaporation times.
机译:本文将讨论微重力分析和测试的状态,以开发热熔压实机(HMC)。由于流体在微重力下的行为完全不同,因此HMC的蒸发过程预计将与1-g不同。开发了一个热模型来支持HMC的设计和操作。此外,还描述了低重力飞行器的飞行数据,以评估在微重力操作过程中可能将水从HMC中挤出的点。为了使HMC达到最佳的传热效果,应在任何水离开HMC之前停止压实过程,但仍应设法尽可能地压实以引起高的传热,从而缩短蒸发时间。

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