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Experimental Elaboration of Liquid Droplet Cooler-Radiator Models under Microgravity and Deep Vacuum Conditions

机译:在微重力和深真空条件下液滴冷却器-散热器模型的实验阐述

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摘要

The basic results of space tests of liquid droplet cooler-radiator models as the main elements of frameless systems for low-grade heat rejection are considered. The studies carried out have been analyzed and intermediate elaboration's results are summarized, which concern (1) the development of generators of droplet propellant flows, (2) revealing an operational behavior of fluid collectors of various types and analysis of unsolved problems associated with droplet collection upon the open trajectory's section passage, and (3) provision of the coolant circulation contour's closing. The necessity is substantiated for the activization of works directed to carrying out space experiments with improved radiator models and new promising propellants in order to provide a possibility of creating new space power plants characterized by megawatt power levels.
机译:考虑了液滴冷却器-散热器模型的空间测试的基本结果,该模型是无框架低品位散热系统的主要元素。分析了所进行的研究并总结了中间阐述的结果,这些结果与(1)液滴推进剂流发生器的发展有关,(2)揭示了各种类型的流体收集器的运行行为以及与液滴收集有关的未解决问题的分析(3)冷却液循环轮廓的关闭。证实了有必要通过改进的辐射器模型和新的有前途的推进剂来激活旨在进行空间实验的工作,以便提供建立具有兆瓦级功率水平的新型空间发电厂的可能性。

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