Generative Design of a Novel Additively Manufactured Solar Array System for Powering Space Equipment on the Lunar Surface

J. Rios, Carlos Velázquez, Teddy Rakotomanana, M. Kabir, Jiajun Xu
{"title":"Generative Design of a Novel Additively Manufactured Solar Array System for Powering Space Equipment on the Lunar Surface","authors":"J. Rios, Carlos Velázquez, Teddy Rakotomanana, M. Kabir, Jiajun Xu","doi":"10.1115/imece2021-71221","DOIUrl":null,"url":null,"abstract":"\n The moon poses harsh conditions including excessively cold 14-day nights in some locations. However, the South Pole of the moon receives sunlight 100% of the time in summer and 70% of the time in Winter. NASA is, therefore, seeking to land at the South Pole by 2024 under Artemis missions and deploy solar arrays to power landers, rovers, and other equipment in order to facilitate a sustainable presence on the moon. Artemis project also seeks to lay the groundwork for a crewed mission to the Mars. To meet the NASA needs for Artemis mission, the desired solar array system is required to cover a large surface area to maximize the capture of solar irradiance when the arrays are deployed 10 meters above the lunar terrain. Additionally, the design must be lightweight, capable of being redeployed and retracted with minimal human interaction, and can withstand lunar dust, radiation, and extreme temperatures. In the present study, a scale-down working model of the prototype (1:10th scale) is introduced with a particular emphasis on the mechanical mechanisms of telescopic boom, tower, and deployment/retraction of solar arrays. The solar arrays are encased in a cylinder that sits atop the telescopic boom and can be deployed irrespective of the boom height. This study attempts to use principles of Geometric Origami to create a novel structural design that allows for a large-diameter array to be rigid without a supporting skeletal structure. By removing the rigid supporting structure, the design becomes highly portable and easily packable and deployable. Once the design is finalized, Fusion360’s Generative Design Suite will be used to optimize the strength-to-weight ratio and manufacturability. Conducting topology optimization based on finite element modeling to meet the required criteria on the weight, strength, durability, and rigidity leads often to irregular geometries which are not possible to be fabricated using conventional manufacturing. However, additive manufacturing features the ability to develop and fabricate the proposed innovative design.","PeriodicalId":187039,"journal":{"name":"Volume 9: Engineering Education","volume":"32 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Volume 9: Engineering Education","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1115/imece2021-71221","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

Abstract

The moon poses harsh conditions including excessively cold 14-day nights in some locations. However, the South Pole of the moon receives sunlight 100% of the time in summer and 70% of the time in Winter. NASA is, therefore, seeking to land at the South Pole by 2024 under Artemis missions and deploy solar arrays to power landers, rovers, and other equipment in order to facilitate a sustainable presence on the moon. Artemis project also seeks to lay the groundwork for a crewed mission to the Mars. To meet the NASA needs for Artemis mission, the desired solar array system is required to cover a large surface area to maximize the capture of solar irradiance when the arrays are deployed 10 meters above the lunar terrain. Additionally, the design must be lightweight, capable of being redeployed and retracted with minimal human interaction, and can withstand lunar dust, radiation, and extreme temperatures. In the present study, a scale-down working model of the prototype (1:10th scale) is introduced with a particular emphasis on the mechanical mechanisms of telescopic boom, tower, and deployment/retraction of solar arrays. The solar arrays are encased in a cylinder that sits atop the telescopic boom and can be deployed irrespective of the boom height. This study attempts to use principles of Geometric Origami to create a novel structural design that allows for a large-diameter array to be rigid without a supporting skeletal structure. By removing the rigid supporting structure, the design becomes highly portable and easily packable and deployable. Once the design is finalized, Fusion360’s Generative Design Suite will be used to optimize the strength-to-weight ratio and manufacturability. Conducting topology optimization based on finite element modeling to meet the required criteria on the weight, strength, durability, and rigidity leads often to irregular geometries which are not possible to be fabricated using conventional manufacturing. However, additive manufacturing features the ability to develop and fabricate the proposed innovative design.
一种新型增材制造月球表面空间设备太阳能阵列供电系统的生成设计
月球带来了恶劣的环境,包括在一些地方极度寒冷的14天夜晚。然而,月球的南极在夏季有100%的时间接受阳光,在冬季有70%的时间接受阳光。因此,美国宇航局正寻求在2024年之前在阿尔忒弥斯任务下登陆南极,并部署太阳能电池阵列为着陆器、漫游者和其他设备供电,以促进在月球上的可持续存在。阿尔忒弥斯计划还试图为载人火星任务奠定基础。为了满足NASA对Artemis任务的需求,当阵列部署在月球地形上方10米处时,所需的太阳能阵列系统需要覆盖较大的表面积,以最大限度地捕获太阳辐照度。此外,设计必须轻巧,能够在最少的人为影响下重新部署和收缩,并且能够承受月球尘埃、辐射和极端温度。在本研究中,介绍了原型机的按比例缩小的工作模型(1:10比例),并特别强调了伸缩臂、塔架和太阳能电池阵列的展开/收缩的机械机制。太阳能电池阵列被封装在一个圆柱体中,圆柱体位于伸缩臂的顶部,无论臂的高度如何,都可以展开。本研究试图利用几何折纸的原理来创造一种新颖的结构设计,这种设计允许大直径阵列在没有支撑骨架结构的情况下保持刚性。通过去除刚性支撑结构,该设计变得高度便携,易于包装和部署。一旦设计完成,将使用Fusion360的生成设计套件来优化强度重量比和可制造性。基于有限元建模进行拓扑优化,以满足重量、强度、耐久性和刚度的要求,往往导致不规则的几何形状,这是传统制造方法无法制造的。然而,增材制造具有开发和制造所提出的创新设计的能力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信