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Environmental Verification of NASA's Europa Clipper Mission

机译:美国宇航局欧罗巴-克利伯号任务的环境验证

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NASA's Jet Propulsion Laboratory (JPL) and its partner are planning a mission to explore an icy moon of Jupiter, Europa. The objective of the planned Europa Clipper mission is to gain insight into the key ingredients for this potentially habitable world. This mission will conduct investigations using a suite of remote sensing and in-situ fields and particles instruments, and a two-channel ice-penetrating radar. Among its science objectives are to produce high-resolution images of Europa's surface, determine its composition, look for signs of recent or ongoing activity, measure the thickness of the ice shell, search for subsurface lakes, and determine the depth and salinity of Europa's ocean. Europa Clipper is expected to encounter very challenging environments. These environments include radiation, dynamics, thermal, and electromagnetics, which have been translated into a set of environmental requirements that are levied onto the Europa Clipper flight system design. This paper describes how the environmental requirements are specified and verified for each flight component and at which level of integration. A couple of examples will be provided to illustrate the process by which a comprehensive set of verification activities is specified and performed for individual subsystems and instruments to ensure mission success.
机译:美国宇航局喷气推进实验室(JPL)及其合作伙伴正在计划一项任务,探索木卫二木星上的一颗冰卫星。计划中的欧罗巴-克利伯号任务的目标是深入了解这个潜在宜居世界的关键要素。该任务将使用一套遥感和现场场与粒子仪器,以及一台双通道探冰雷达进行调查。其科学目标之一是制作木卫二表面的高分辨率图像,确定其组成,寻找最近或正在进行的活动迹象,测量冰层厚度,搜索地下湖泊,并确定木卫二海洋的深度和盐度。欧罗巴克利伯号预计将遇到非常具有挑战性的环境。这些环境包括辐射、动力学、热学和电磁学,这些环境已经转化为一系列环境要求,这些要求被施加到欧罗巴克利伯号飞行系统的设计中。本文描述了如何为每个飞行部件规定和验证环境要求,以及在哪个集成级别。将提供两个示例来说明为确保任务成功而为单个子系统和仪器指定和执行的一整套验证活动的过程。

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