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SELECTING MATERIALS TO PROTECT INFLATABLE STRUCTURES FROM THE SPACE ENVIRONMENT

机译:选择材料以保护空间环境中的不可膨胀结构

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The selection of candidate inflatable structures for future manned space exploration is driven by the materials’ resistance to the hostile space environment. After a detailed analysis of the system level requirements, a thorough characterization of innovative flexible materials with proper structural and environmental performance is being performed. Using the selected materials, lightweight flexible shields fully integrated in the inflatable structures are under development to provide protection from Micro- Meteoroids and Orbital Debris (MMOD) impacts. Hypervelocity impact tests with Light Gas Gun are ongoing onto targets simulating inflatable structures composed of thermal protection, MMOD shields, pressure and air containment. The evaluation of shielding efficiency against the trapped, solar and cosmic radiation environment is on-going based on short and long term shielding experiments aboard ISS (ESCHILO, ALTCRISS, SOFOCLE), on dedicated tests in accelerators and on Montecarlo simulations. The candidate materials are compared with the typical rigid materials used in current spacecraft, to optimise and validate the radiation shielding solutions.
机译:材料对敌对太空环境的抵抗力驱使了人们选择用于未来载人太空探索的可充气结构。在对系统级别要求进行详细分析之后,将对具有适当结构和环境性能的创新柔性材料进行全面表征。使用选定的材料,正在开发完全集成在可充气结构中的轻质柔性防护罩,以保护免受微型流星体和轨道碎片(MMOD)的影响。正在用轻型气枪进行超高速冲击试验,以模拟由热保护,MMOD防护罩,压力和空气密闭组成的可充气结构的目标。根据国际空间站(ESCHILO,ALTCRISS,SOFOCLE)上短期和长期的屏蔽实验,加速器的专用测试以及蒙特卡洛模拟,正在进行针对被困的太阳和宇宙辐射环境的屏蔽效率评估。将候选材料与当前航天器中使用的典型刚性材料进行比较,以优化和验证辐射屏蔽解决方案。

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