The planetary protection strategy of Mars Sample Return’s Earth Return Orbiter mission

IF 1 Q3 ENGINEERING, AEROSPACE Journal of Space Safety Engineering Pub Date : 2024-06-01 DOI:10.1016/j.jsse.2024.04.013
Giuseppe Cataldo , Lorenz Affentranger , Brian G. Clement , Daniel P. Glavin , David W. Hughes , John Hall , Bruno Sarli , Christine E. Szalai
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Abstract

The Mars Sample Return campaign aims to use three flight missions and one ground element to safely bring rock cores, regolith and atmospheric samples from the surface of Mars to Earth to answer key questions about the geologic and climate history of Mars, including the potential for ancient life. Since its landing in Jezero Crater in 2021, the first mission, NASA’s Mars 2020, has collected a number of samples on the crater floor and on the delta using the Perseverance rover. Subsequent missions would recover the sealed sample tubes, launch them into Mars orbit, and transport them back to Earth. The ground element would be a high-containment facility that would isolate and protect the samples during initial sample characterization, which would include sample safety assessments and time-sensitive scientific investigations. These elements are currently in the planning and design stages of development, and represent an international effort of NASA, the European Space Agency (ESA), and many industry partners. The work presented here provides an overview of the planetary protection strategy of the third flight mission, the ESA-led Earth Return Orbiter, which hosts the NASA-provided Capture, Containment, and Return System. The orbiter would detect and capture the container with up to 30 sealed tubes previously put in Martian orbit, contain them in redundant containers to ensure that no potentially hazardous Mars particles are released, and return them to Earth through an entry vehicle. Both NASA and ESA policies comply with the United Nations’ Outer Space Treaty by planning to protect Earth’s biosphere from any potential adverse effects from material returned from solar system bodies beyond the Earth-Moon system. In the conduct of Mars Sample Return, the two agencies have mutually agreed to apply approaches consistent with their own planetary protection standards to the campaign elements they each provide.

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火星取样返回地球轨道飞行器任务的行星保护战略
火星样本送回活动旨在利用三次飞行任务和一次地面任务,将火星表面的岩芯、碎屑岩和大气样本安全地送回地球,以回答有关火星地质和气候历史的关键问题,包括存在远古生命的可能性。自 2021 年在杰泽罗陨石坑着陆以来,第一个任务,即 NASA 的 "火星 2020",已经利用 "坚毅 "漫游车在陨石坑底部和三角洲收集了一些样本。随后的任务将回收密封的样本管,将其发射到火星轨道,并运回地球。地面部分将是一个高度封闭的设施,在最初的样本特征描述期间对样本进行隔离和保护,其中包括样本安全评估和具有时间敏感性的科学调查。这些元素目前正处于开发的规划和设计阶段,代表了美国国家航空航天局(NASA)、欧洲航天局(ESA)和许多行业合作伙伴的国际努力。本文介绍的工作概述了第三次飞行任务(欧空局领导的地球返回轨道器)的行星保护战略,该轨道器载有美国航天局提供的捕获、遏制和返回系统。该轨道器将探测并捕获先前置于火星轨道上的装有多达 30 个密封管的容器,将其装在冗余容器中以确保不释放潜在危险的火星粒子,并通过进入飞行器将其送回地球。美国航天局和欧空局的政策都符合联合国《外层空间条约》的规定,计划保护地球生物圈免受从地月系统以外的太阳系天体返回的物质可能造成的任何不利影响。在进行火星取样返回时,这两个机构共同商定对各自提供的活动内容采用符合其各自行星保护标准的方法。
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来源期刊
Journal of Space Safety Engineering
Journal of Space Safety Engineering Engineering-Safety, Risk, Reliability and Quality
CiteScore
2.50
自引率
0.00%
发文量
80
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Editorial Board An economic indicator of the orbital debris environment Adaptive relative orbit control considering laser ablation uncertainty Post mission disposal of Megha-Tropiques-1 through controlled atmospheric Re-entry to be published in: The journal of space safety engineering Development of ballistic limit equations in support of the Mars sample return mission
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