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Advanced Space Suit Portable Life Support Subsystem Packaging Design

机译:先进的太空服便携式生命支持子系统包装设计

摘要

This paper discusses the Portable Life Support Subsystem (PLSS) packaging design work done by the NASA and Hamilton Sundstrand in support of the 3 future space missions; Lunar, Mars and zero-g. The goal is to seek ways to reduce the weight of PLSS packaging, and at the same time, develop a packaging scheme that would make PLSS technology changes less costly than the current packaging methods. This study builds on the results of NASA s in-house 1998 study, which resulted in the "Flex PLSS" concept. For this study the present EMU schematic (low earth orbit) was used so that the work team could concentrate on the packaging. The Flex PLSS packaging is required to: protect, connect, and hold the PLSS and its components together internally and externally while providing access to PLSS components internally for maintenance and for technology change without extensive redesign impact. The goal of this study was two fold: 1. Bring the advanced space suit integrated Flex PLSS concept from its current state of development to a preliminary design level and build a proof of concept mockup of the proposed design, and; 2. "Design" a Design Process, which accommodates both the initial Flex PLSS design and the package modifications, required to accommodate new technology.
机译:本文讨论了NASA和Hamilton Sundstrand为支持3个未来太空飞行任务而进行的便携式生命支持子系统(PLSS)包装设计工作;月球,火星和零重力。目标是寻求减轻PLSS包装重量的方法,同时开发一种包装方案,使PLSS技术的变更成本低于当前的包装方法。这项研究建立在NASA 1998年内部研究结果的基础上,该研究结果产生了“ Flex PLSS”概念。对于本研究,使用了当前的EMU示意图(低地球轨道),以便工作团队可以专注于包装。 Flex PLSS封装需要:在内部和外部将PLSS及其组件保护,连接和保持在一起,同时在内部提供对PLSS组件的访问以进行维护和技术变更,而不会产生广泛的重新设计影响。这项研究的目的有两个方面:1.将先进的太空服集成Flex PLSS概念从其当前的开发状态提升到初步设计水平,并建立所提议设计的概念模型,以及; 2.“设计”一个设计过程,该过程既包含初始Flex PLSS设计,也包含适应新技术所需的封装修改。

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