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Design, Analysis and Fabrication of Secondary Structural Components for the Habitat Demonstration Unit-Deep Space Habitat

机译:居住示范单位-深空居住区次要结构部件的设计,分析与制作

摘要

In support of NASA s Habitat Demonstration Unit - Deep Space Habitat Prototype, a number of evolved structural sections were designed, fabricated, analyzed and installed in the 5 meter diameter prototype. The hardware consisted of three principal structural sections, and included the development of novel fastener insert concepts. The articles developed consisted of: 1) 1/8th of the primary flooring section, 2) an inner radius floor beam support which interfaced with, and supported (1), 3) two upper hatch section prototypes, and 4) novel insert designs for mechanical fastener attachments. Advanced manufacturing approaches were utilized in the fabrication of the components. The structural components were developed using current commercial aircraft constructions as a baseline (for both the flooring components and their associated mechanical fastener inserts). The structural sections utilized honeycomb sandwich panels. The core section consisted of 1/8th inch cell size Nomex, at 9 lbs/cu ft, and which was 0.66 inches thick. The facesheets had 3 plys each, with a thickness of 0.010 inches per ply, made from woven E-glass with epoxy reinforcement. Analysis activities consisted of both analytical models, as well as initial closed form calculations. Testing was conducted to help verify analysis model inputs, as well as to facilitate correlation between testing and analysis. Test activities consisted of both 4 point bending tests as well as compressive core crush sequences. This paper presents an overview of this activity, and discusses issues encountered during the various phases of the applied research effort, and its relevance to future space based habitats.
机译:为了支持NASA的“人居示范单位-深太空人居原型”,设计,制造,分析并安装了许多演变后的结构截面,直径为5米。硬件包括三个主要的结构部分,并包括新型紧固件嵌件概念的开发。开发的文章包括:1)主地板部分的1/8,2)内半径地板梁支撑,该支撑与(1),3)两个上舱口部分原型连接并支撑(4)新颖的嵌件设计用于机械紧固件附件。在组件的制造中采用了先进的制造方法。结构组件是使用当前的商用飞机构造作为基线(针对地板组件及其相关的机械紧固件插件)开发的。结构部分采用蜂窝夹芯板。核心部分由1/8英寸的单元格Nomex组成,厚度为9磅/立方英尺,厚度为0.66英寸。面板各有3层,厚度为每层0.010英寸,由带有环氧增强材料的机织E玻璃制成。分析活动包括分析模型和初始封闭式计算。进行测试以帮助验证分析模型的输入,并促进测试和分析之间的关联。测试活动包括4点弯曲测试以及压芯挤压顺序。本文概述了这项活动,并讨论了在应用研究工作的各个阶段遇到的问题,以及它与未来基于空间的栖息地的相关性。

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