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Thermal Analysis and Design of an Advanced Space Suit

机译:先进航天服的热分析与设计

摘要

The thermal dynamics and design of an Advanced Space Suit are considered. A transient model of the Advanced Space Suit has been developed and implemented using MATLAB/Simulink to help with sizing, with design evaluation, and with the development of an automatic thermal comfort control strategy. The model is described and the thermal characteristics of the Advanced Space suit are investigated including various parametric design studies. The steady state performance envelope for the Advanced Space Suit is defined in terms of the thermal environment and human metabolic rate and the transient response of the human-suit-MPLSS system is analyzed.
机译:考虑了高级航天服的热力学和设计。已经使用MATLAB / Simulink开发和实现了高级航天服的瞬态模型,以帮助进行尺寸确定,设计评估以及自动热舒适控制策略的开发。描述了模型,并研究了高级航天服的热特性,包括各种参数设计研究。根据热环境和人体新陈代谢率定义了高级太空服的稳态性能范围,并分析了人体服-MPLSS系统的瞬态响应。

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