Research on Integrated Interface Design of Small Modular Spacecraf

Wanxin Man, Xinhong Li, Zhibin Zhang, Jiping An, Guohui Zhang, Junwei He
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Abstract

Modularity in space provides a solution to the scale-constrained problem of space systems, while providing other benefits in terms of flexibility, sustainability and affordability. In the system, modules are added and removed through interconnect interfaces, which transfer mechanical load, data, electrical power, and heat from one module to another. The current research tends to integrate multiple functions into a single device or equipment to reduce costs and improve standardization. This article will explore the design requirements and constraints that need to be satisfied in the design of this standardized, extensible, multifunctional (mechanical, electrical, data, thermal), modular interface, and compare the realization of each function to provide a design consideration.
小型模块化航天器集成接口设计研究
空间模块化为空间系统的规模限制问题提供了解决方案,同时在灵活性、可持续性和可负担性方面提供了其他好处。在系统中,通过互连接口增加和删除模块,将机械负载、数据、电力和热量从一个模块传递到另一个模块。目前的研究倾向于将多种功能集成到单个设备或设备中,以降低成本并提高标准化。本文将探讨在设计这种标准化、可扩展、多功能(机械、电气、数据、热)的模块化接口时需要满足的设计需求和约束,并比较每个功能的实现,以提供设计考虑。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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