多功能支撑结构技术进展

R. John, G. Atxaga, H. Frerker, A. Newerla
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引用次数: 4

摘要

多功能支撑结构(MFSS)技术有望减少航天器(S/C)电子元件的总质量和包装体积。该技术通过将电子、热控制和结构支撑集成到一个单一元素中,消除了电子箱底盘和盒子之间的电缆。MFSS技术的最终目标是减少未来航天器部件的尺寸、重量、功耗、成本和生产时间。本文重点讨论了基于电荷调节器(CR)应用的MFSS技术中与热管理相关的主要挑战和解决方案。从CR的主要热要求开始,论文将包括:基于高导电性碳纤维CFRP的概念和详细设计,热材料样品测试程序的描述和结果,执行的第一次热模拟的参数和结果
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Advancement of Multifunctional support structure technologies (AMFSST)
The multifunctional support structure (MFSS) technology is promising a reduction of overall mass and packing volume for spacecraft (S/C) electronic components. This technology eliminates the electronic box chassis and the cabling between the boxes by integrating the electronics, thermal control and the structural support into one single element The ultimate goal of the MFSS technology is to reduce size, weight, power consumption, cost and production time for future spacecraft components. The paper focus on the main challenges and solutions related to the thermal management within the MFSS technology based on the selected charge regulator (CR) application. Starting with the main set of thermal requirements for the CR the paper will include: Conceptual and detailed design based on high-conductivity carbon fibre CFRP, Description and results of the thermal material sample test program, Parameter and results for the performed first thermal simulation
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