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Development of the miniature spacecraft energy retention (MiSER) thermal control panel

机译：开发微型航天器能量保留（MISER）热控制面板

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Over the past two years, Starsys and The Johns Hopkins University Applied Physics Laboratory (APL) have been working toward the development of a thermal panel that uses a spacecraft's internal power to control its temperature. The panel incorporates two different thermal technologies: a thermal switch and a high conductivity composite radiator. While thermal switches have been used before, the design and testing costs associated with each new design make them an undesirable alternative. The MiSER panel incorporates a fully tested thermal switch with a radiator into a modular system that can be easily added onto any spacecraft structure. The lightweight radiator makes it self-supporting, so interfaces with the mounting structure are simplified. The same panel can provide thermal control over a wide range of environmental conditions, making constellation spacecraft viable with significantly different orbits. The paper discusses the development of the MiSER panel and the analysis and testing done to quantify the performance of the system.
机译：在过去的两年里，STARSYS和Johns Hopkins大学应用物理实验室（APL）一直致力于开发一个使用宇宙飞船的内部电力来控制其温度的热面板。该面板采用两种不同的热技术：热开关和高导电性复合散热器。虽然以前使用了热交换机，但与每个新设计相关的设计和测试成本使其成为一个不期望的替代品。 MARER面板采用完全测试的热开关，其具有散热器进入模块化系统，该系统可以容易地添加到任何航天器结构上。轻质散热器使其自支撑，因此简化了安装结构的接口。同一面板可以在各种环境条件下提供热控制，使星座航天器具有显着不同的轨道。本文讨论了纪要面板的发展和分析和测试，以量化系统的性能。

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