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Design development of an inflatable module for a Lunar/Martian base

机译:设计月球/火星基地充气模块的开发

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The most notable aspect of the Lunar and Martian environments is the lack of a substantial atmosphere. Atmospheric pressure on the Moon is essentially zero, and is very low on Mars. Support of human occupancy requires an internal atmosphere and, therefore, the most efficient structure is an inflatable tensile membrane. A generic inflatable module is proposed as an efficient and functional structure for a Lunar/Martian base. Each module consists of thin membranes supported by a framing system composed of cylindrical arches and columns. The framing system maintains the module shape and supports the deflated module. Three options for the framing systems were evaluated. Membrane sleeves filled with structural foam, rigid members made of either titanium or graphite/epoxy composite, and pressurized membrane tubes were evaluated. The pressurized membrane tubes were found to have the lowest mass and be sufficient for supporting the structure. A structural analysis was performed using a three-dimensional (3D) computer simulation. Results from the structural analysis were applied to improve the structural design of the module.
机译:农历和火星环境中最值得注意的方面是缺乏大量氛围。月球上的大气压基本上为零,在火星上非常低。支持人类入住需要内部大气,因此,最有效的结构是充气抗拉膜。普通充气模块被提出为月球/火星基地的有效和功能结构。每个模块由由圆柱形拱门和列组成的框架系统支撑的薄膜组成。框架系统保持模块形状并支持放气模块。评估了框架系统的三个选项。膜套装填充有结构泡沫,评价由钛或石墨/环氧复合材料制成的刚性构件以及加压膜管。发现加压膜管具有最低质量并且足以用于支撑结构。使用三维(3D)计算机模拟进行结构分析。采用结构分析的结果应用于改善模块的结构设计。

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