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Design and modeling of a Mars space suit.

机译:火星太空服的设计和建模。

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This study investigates a light-weight design for a space suit and life support system for astronauts to wear in the exploration of Mars. Existing space suit designs for the Moon and Earth orbit are far too heavy for use on Mars. The portable life support system makes up the majority of the weight in current designs, and is the focus for reducing suit weight. This study explores the concept of using a selectively permeable membrane as the suit's pressure-retaining structure while serving as a replacement for the complex conventional systems for controlling heat and humidity. Current suits use active systems to maintain the suit temperature, cool the astronaut, and control humidity in the suit air. Heat is rejected to the outside by sublimation of ice to the vacuum. The life support system bypasses the body's natural regulatory capability. Using a selectively permeable membrane allows water vapor to permeate through the pressure retaining bladder and diffuse through the layers of the suit directly to the Mars atmosphere; this system dehumidifies the air and allows the body's own thermal regulation system to cool the astronaut by evaporation of sweat. Modular insulation can be added and removed for comfort, much as a jacket is used on Earth.; A mathematical model was developed to simulate the heat and mass transfer characteristics of the human, the layered suit including selectively permeable pressure bladder and variable insulation, and the Mars environment. The model incorporates metabolic data collected in Leslie Wickman's experiments on walking and running with various loads in simulated reduced gravity. Simulation results for several exploration scenarios are presented, covering the full range of conditions that the first Mars astronauts are likely to encounter. Under all environmental conditions and work loads, the astronaut can maintain a comfortable temperature with moderate sweating by adjusting the modular insulation. A related use of membranes controls carbon dioxide in the suit, replacing the use of a lithium hydroxide scrubber. These systems reduce the life support system mass enough to make a suit light enough for easy mobility on Mars.
机译:这项研究调查了宇航员在探索火星时所穿的宇航服和生命支持系统的轻型设计。现有的月球和地球轨道太空服设计过于沉重,无法在火星上使用。便携式生命支持系统占当前设计的大部分重量,并且是减轻西服重量的重点。这项研究探索了使用选择性渗透膜作为西服的压力保持结构,同时替代用于控制热量和湿度的复杂常规系统的概念。当前的西服使用主动系统来维持西服温度,冷却宇航员并控制西服空气中的湿度。通过将冰升华至真空,将热量排到外部。生命支持系统会绕过人体的自然调节能力。使用选择性渗透的膜可以使水蒸气渗透通过保压气囊,并扩散穿过衣服的各层,直接进入火星大气层。该系统为空气除湿,并允许人体自身的温度调节系统通过汗液的蒸发来冷却宇航员。模块化的绝缘层可以增加或去除以增加舒适感,就像在地球上使用夹克一样。建立了一个数学模型来模拟人体的传热和传质特性,包括选择性渗透压力的压力囊和可变隔热层的分层服以及火星环境。该模型结合了莱斯利·威克曼(Leslie Wickman)在模拟重力降低的各种负荷下行走和奔跑的实验中收集的代谢数据。给出了几种探索方案的模拟结果,涵盖了首批火星宇航员可能遇到的所有条件。在所有环境条件和工作负荷下,宇航员都可以通过调节模块化绝缘来维持适度的温度和适度的出汗。膜的相关用途可控制衣服中的二氧化碳,从而代替氢氧化锂洗涤器的用途。这些系统减少了生命支持系统的重量,足以使西装足够轻,便于在火星上移动。

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