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Development and design of multifunctional lightweight structures for satellite applications

机译:卫星应用多功能轻质结构的开发与设计

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Within the framework of the German national project multiSat multifunctional composite structures for satellite applications are developed. The objective is the integration of passive and active functions into the load-bearing spacecraft structure by using suitable materials, components and mechanisms. The passive functions are heat transfer, radiation shielding and protection against orbital debris impact, whereas the active functions include vibration suppression and transmission of data and electrical energy. Composite materials and structures usually consist of multiple layers which makes them suitable for functional integration since each layer can be defined and designed to provide one or more specific functions. The concept of a multifunctional structure allows for the reduction of the overall satellite mass and of installation space required for subsystems. It also opens up new opportunities for highly integrative and standardized production processes and lower total costs and time for manufacturing, qualification and launch. Composite sandwich panels are investigated as representative structural components of a satellite. Based on a conceptual analysis, a design of a multifunctional composite sandwich panel is developed. Various materials and layups are investigated in order to implement the passive functions and enable the integration of tertiary structures for the active functions. The heat transfer within the structure is improved by the use of structural materials with high thermal conductivities and radiation shielding is enhanced by layers with high radiation absorption capability. Metallic lattice structures and high-strength fabrics are integrated into the core of the sandwich in order to effectively break up and slow down impacting debris particles. Vibration reduction is achieved by means of flat piezoelectric transducers bonded to the face sheets and connected to shunt circuits, whereas flat electric cables and optical fibres are embedded into th
机译:在德国国家项目的框架内,开发了用于卫星应用的多功能复合结构。目的是通过使用合适的材料,组件和机制将被动和主动功能集成到承载航天器结构中。被动功能是传热,辐射屏蔽和防止轨道碎片的影响,而主动功能包括振动抑制和数据和电能传输。复合材料和结构通常由多个层组成,这使得它们适合于功能集成,因为可以定义和旨在提供一种或多种特定功能。多功能结构的概念允许减少整体卫星质量和子系统所需的安装空间。它还为高度综合和标准化的生产流程开辟了新的机会,以及降低制造,资格和发布的总成本和时间。复合夹层面板被研究为卫星的代表性结构组分。基于概念分析,开发了多功能复合夹层板的设计。研究了各种材料和上篮,以便实现被动功能并实现第三级结构的积分进行活动功能。通过使用具有高导热性的结构材料,通过具有高辐射吸收能力的层增强了结构材料的热传递得到改善。金属晶格结构和高强度织物被整合到三明治的核心中,以有效地分解并减慢冲击碎片颗粒。通过粘合到面板的扁平压电换能器实现振动减小,并连接到分流电路,而平坦的电缆和光纤嵌入到其中

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