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Assessments of the impacts of orbital fragmentations using the Near-Earth Orbital Debris Environment Evolutionary Model (NEODEEM) 利用近地轨道碎片环境演变模型评估轨道碎裂的影响
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.07.008
Ryusuke Harada , Satomi Kawamoto , Toshiya Hanada
This study evaluates the environmental impacts of orbital fragmentation such as an anti-satellite test, collision between two objects, and explosion. A debris environment evolutionary model named NEODEEM, jointly developed by Kyushu University and JAXA, is used to predict future populations and calculate collision probabilities after a fragmentation. This study focuses on characteristics of the fragmented objects, such as altitude, mass, and whether they belong to a Large Constellation (LC). When a fragmentation occurs at higher altitudes, the new fragments will remain in orbit for a long time. Due to this accumulation, the fragments will not only keep the number of objects and probability of collision higher but also cause the risk of secondary collisions between fragments and background objects. When a collision occurs inside an LC at a lower altitude, the impacts will be short-term because most of fragments decay quickly. However, the number of conjunctions, i.e., operational roads, will increase rapidly because many satellites are operated at the same altitude. This study also discusses a collision probability to an LC taking into account the small size of fragments larger than 1 cm.
这项研究评估了反卫星试验、两个物体之间的碰撞和爆炸等轨道碎裂对环境的影响。九州大学和日本宇宙航空研究开发机构联合开发了一个名为 NEODEEM 的碎片环境演化模型,该模型用于预测未来的碎片群并计算碎片发生后的碰撞概率。这项研究的重点是碎裂物体的特征,如高度、质量以及是否属于大型星座(LC)。当碎裂发生在较高的高度时,新的碎片会在轨道上停留很长时间。由于这种积累,碎片不仅会使天体数量和碰撞概率保持在较高水平,还会造成碎片与背景天体发生二次碰撞的风险。当碰撞发生在高度较低的低地球轨道内时,由于大部分碎片衰变较快,因此碰撞将是短期的。然而,由于许多卫星在同一高度运行,会合(即运行道路)的数量将迅速增加。考虑到大于 1 厘米的碎片体积较小,本研究还讨论了与低地球轨道的碰撞概率。
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引用次数: 0
AstroLibrary: A library for real-time conjunction assessment and optimal collision avoidance AstroLibrary:用于实时会合评估和优化避免碰撞的图书馆
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.07.003
Shawn SH Choi , Peter JH Ryu , Kyuil Sim , Jaedong Seong , Jae Wook Song , Misoon Mah , Douglas DS Kim
Geospace is crowded due to the proliferation of satellites and space debris and will become more crowded with the increasing deployment of new space missions. This trend is rapidly increasing the probability of collisions between space objects. Space objects fly at extreme speeds; hence, the consequences of collisions are catastrophic. However, accurate and efficient conjunction assessment (CA) and collision avoidance (COLA) have long been challenging, even with the current space catalogues of O(104) size. As the space catalogue size increases owing to the increased number of new satellites, improved sensor capabilities, and Kessler syndrome, the situation will worsen unless a paradigm-transforming computational method is devised. Here, we present the SpaceMap method, which can perform real-time CA and near-real-time COLA for O(106) or more objects, provided that the spatiotemporal proximity amongst satellites is represented in a Voronoi diagram. As the most concise and efficient data structure for spatiotemporal reasoning amongst moving objects, Voronoi diagrams play a key role in the mathematical and computational basis for a new genre of artificial intelligence (AI) called space–time AI, which can find the best solutions to CA/COLA and other space decision-making problems in longer timeline windows. The algorithms are implemented in C++ and are available on GitHub as AstroLibrary, which has RESTful APIs and Python packages that can be called from application programs. Using this library, anyone with elementary programming skills can easily develop efficient applications for challenging spatiotemporal problems.
由于卫星和空间碎片的激增,地球空间变得十分拥挤,而且随着新的空间飞行任务的不断部署,地球空间将变得更加拥挤。这一趋势正在迅速增加空间物体之间发生碰撞的概率。空间物体的飞行速度极快,因此碰撞的后果是灾难性的。然而,长期以来,精确高效的会合评估(CA)和碰撞避免(COLA)一直是一项挑战,即使是在当前 O(104)大小的空间目录中也是如此。随着新卫星数量的增加、传感器能力的提高以及凯斯勒综合征(Kessler Syndrome)的出现,空间目录的规模也在不断扩大,除非设计出一种能改变模式的计算方法,否则情况将会恶化。在此,我们提出了 SpaceMap 方法,该方法可以对 O(106) 或更多的对象执行实时 CA 和近实时 COLA,前提是卫星之间的时空接近性用 Voronoi 图表示。作为移动物体间时空推理最简洁、最高效的数据结构,Voronoi 图在被称为时空人工智能(space-time AI)的人工智能(AI)新流派的数学和计算基础中发挥着关键作用,它能在更长的时间窗口内找到 CA/COLA 和其他空间决策问题的最佳解决方案。这些算法是用 C++ 实现的,并以 AstroLibrary 的形式发布在 GitHub 上,它有 RESTful API 和 Python 包,可以从应用程序中调用。利用这个库,任何具备初级编程技巧的人都能轻松开发出高效的应用程序,解决具有挑战性的时空问题。
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引用次数: 0
Evaluation of low earth orbit post-mission disposal measures 对低地球轨道飞行任务后处置措施的评价
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.03.008
Hugh G. Lewis, Vyara Yazadzhiyan
The substantial benefits arising from the widespread adoption of post-mission disposal in low Earth orbit (LEO) are reflected in a reduced orbital debris population and a reduced frequency of collisions. The benefits are generally seen at higher altitudes whereas some drawbacks in the form of enhanced collision risks have been predicted for lower altitudes. These drawbacks are generally expected to reduce as the post-mission disposal lifetime decreases, as less time at lower altitudes reduces collision probability. This is the rationale used by the Federal Communications Commission (FCC) for its new 5-year rule. To investigate the potential benefits and drawbacks, the DAMAGE computational model was used to investigate the effects of a variety of LEO post-mission disposal rules, including the new 5-year rule, within scenarios involving the deployment of large constellations of satellites. The results suggest substantial reductions in conjunction rates overall, as the post-mission residual orbital lifetime decreases, but indicate an increasing frequency of conjunctions and a corresponding need for risk mitigation maneuvers at low altitudes. The results reinforce the recommendation that disposal must be completed as soon as practicable following end of mission. Additionally, the results highlight the need for careful consideration and further research into post-mission disposal where a residual orbital lifetime is permitted.
在低地球轨道(LEO)广泛采用任务后处置所产生的巨大惠益反映在轨道碎片数量的减少和碰撞频率的降低上。这些益处通常在较高的高度出现,而在较低的高度则会出现一些缺点,即碰撞风险增加。这些缺点一般会随着任务后处置寿命的缩短而减少,因为在较低高度的时间减少了碰撞概率。这也是美国联邦通信委员会(FCC)制定新的 5 年规则的依据。为了研究潜在的益处和弊端,我们使用 DAMAGE 计算模型,在涉及部署大型卫星群的情况下,研究了包括新的 5 年规则在内的各种低地轨道任务后处置规则的影响。结果表明,随着任务后剩余轨道寿命的减少,会合率总体上大幅下降,但表明会合频率越来越高,因此需要在低空采取相应的风险缓解措施。这些结果加强了任务结束后必须在可行的情况下尽快完成处置的建议。此外,结果还突出表明,在允许有剩余轨道寿命的情况下,有必要认真考虑和进一步研究任务结束后的处置问题。
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引用次数: 0
An economic indicator of the orbital debris environment 轨道碎片环境的经济指标
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.04.014
The continued growth of orbital debris increases potential losses faced by commercial operators in Earth's orbits. Yet, there is no commonly accepted measure that describes the orbital debris environment from an economic perspective. This study begins to fill that gap by developing an Orbital Debris Economic Loss Index (ODELI) that measures and tracks the changes in the expected negative economic impact of orbital debris on satellite operators, both in aggregate and in specific orbits. Such information is valuable to the stakeholders, such as policymakers, commercial operators, and the public, in communicating valuable information about the economic state of the orbital debris environment.
We illustrate the calculation of the index utilizing the data from 2012 to 2022. The analysis is based on the publicly available data and the Meteoroid and Space Debris Terrestrial Environment Reference (MASTER) orbital debris environment model. Our analysis suggests that the aggregate expected economic damage to Earth's orbits is increasing at a slower rate than the growth rate of the number of satellites or trackable pieces of debris objects. The slower rate of growth in ODELI indices from 2012 to 2022 is explained by a decrease in the average mass of satellites, a reduction in the real cost of placing satellites in orbit, and a commercial preference to launch satellites into orbits with lower debris density.
The estimates of annual expected economic losses from debris collisions increased from $86 million to $107 million from 2012 to 2022, and the losses are concentrated in the low-Earth orbit (LEO). However, LEO had the smallest rate of increase in ODELI compared to other orbits. Medium-Earth orbit (MEO), which has the smallest contribution to the combined expected economic losses from debris on the Earth's orbits, experienced the fastest rate of increase in ODELI during the same period.
轨道碎片的持续增长增加了地球轨道上商业运营商面临的潜在损失。然而,目前还没有公认的从经济角度描述轨道碎片环境的衡量标准。本研究通过开发轨道碎片经济损失指数(ODELI)开始填补这一空白,该指数可测量和跟踪轨道碎片对卫星运营商的预期负面经济影响的变化,包括总体影响和特定轨道影响。这些信息对于政策制定者、商业运营商和公众等利益相关者来说非常有价值,可以传递有关轨道碎片环境经济状况的宝贵信息。我们利用 2012 年至 2022 年的数据对指数的计算进行了说明。分析基于公开数据和流星体和空间碎片地面环境参考(MASTER)轨道碎片环境模型。我们的分析表明,对地球轨道的总体预期经济损失的增长速度低于卫星或可跟踪碎片物体数量的增长速度。2012 年至 2022 年,ODELI 指数的增长速度较慢,原因是卫星的平均质量下降,将卫星送入轨道的实际成本降低,以及商业上倾向于将卫星发射到碎片密度较低的轨道。不过,与其他轨道相比,低地轨道的 ODELI 增长率最小。中地轨道(MEO)在地球轨道碎片造成的综合预期经济损失中占比最小,但同期的ODELI增长速度最快。
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引用次数: 0
Post mission disposal of Megha-Tropiques-1 through controlled atmospheric Re-entry to be published in: The journal of space safety engineering 通过受控大气重返大气层对 Megha-Tropiques-1 进行飞行任务后处置,将在《空间安全工程》杂志上发表:空间安全工程学杂志
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.05.006
Controlled Re-Entry Experiment of Megha-Tropiques 1 (CREEM), an immensely challenging and significant exercise, was successfully executed on 7 March 2023 by Indian Space Research organization (ISRO) as part of its ongoing efforts to improve compliance with internationally accepted space debris mitigation guidelines. In this paper, we present the overall strategy of CREEM which was primarily shaped by the stringent requirements of targeted impact within a pre-designated zone and ensuring visibility during the final de-boosting burns. We specifically address how the strategy was driven by the on-board and operational constraints, the rationale for the selection of the target region, the de-orbiting maneuver performance details, and the operational workarounds to ensure required subsystem performance. The external coordination related aspects and the lessons learnt are also presented.
印度空间研究组织(ISRO)于 2023 年 3 月 7 日成功执行了 Megha-Tropiques 1 号受控再入大气层实验(CREEM),这是一项极具挑战性的重大演习,也是该组织为更好地遵守国际公认的空间碎片减缓准则而持续努力的一部分。在本文中,我们介绍了 CREEM 的总体战略,该战略主要是根据在预先指定的区域内进行目标撞击和确保在最后的去助推燃烧期间的能见度的严格要求制定的。我们具体讨论了机载和运行限制如何驱动该战略、选择目标区域的理由、离轨机动性能细节以及确保所需子系统性能的运行变通方法。此外,还介绍了与外部协调有关的方面和吸取的经验教训。
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引用次数: 0
An approach to shape parameterization using laboratory hypervelocity impact experiments 利用实验室超高速撞击实验进行形状参数化的方法
IF 1 Q3 ENGINEERING, AEROSPACE Pub Date : 2024-09-01 DOI: 10.1016/j.jsse.2024.05.004
John H. Seago , Heather Cowardin , Phillip Anz-Meador , Alyssa Manis , Joshua Miller , Eric Christiansen
NASA's Orbital Debris Program Office relies on laboratory-based impact tests to supplement the measurement data of on-orbit events that define the orbital debris environment. These experiments deliver information that is essential to interpreting the radar and optical measurements of orbital fragmentation events into useful metrics, such as characteristic size, and to providing a better understanding of the distributions of fragment populations in terms of their masses, material constituents, fragment densities, cross-sectional areas, area-to-mass ratios, shapes, etc. The Satellite Orbital Debris Characterization Impact Test was a notable laboratory impact experiment conducted in 1992 using a surplus U.S. Navy Transit navigation satellite of the 1960s. The data from this ground-based experiment were combined with on-orbit measurements to develop the NASA Standard Satellite Breakup Model (SSBM). To account for advancements in satellite design and construction since, a new impact test series – DebriSat – was conducted in 2014. This test utilized a high-fidelity mock-up spacecraft that better represents the materials and construction techniques used to design and manufacture modern spacecraft. Together, these tests offer valuable data to model an orbital debris environment composed of legacy and modern spacecraft. This paper presents an overview of the two laboratory impact tests, comparing their fragment parameter distributions with each other and with relevant distributions from the NASA SSBM. The categorization and descriptions of fragment shapes are of significant interest for future work, yet there are marked differences in the definitions of shape categories, categorizations of constituent materials, and the measurement techniques employed to populate these two datasets. New rubrics simplify and equate the categorizations between datasets to aid comparative analyses and to facilitate the potential use of both datasets in tandem with future environmental debris models. A preferred approach to classifying shape across disparate datasets uses the characteristic-length dimensions, and a simplified shape classification based on physical, solid-body dimensions, to mathematically construct an encapsulating right-circular cylinder that represents the fragment. The ratio of cylinder length-to-diameter (L:D) then provides a single continuum value for shape that is strongly correlated with its designated shape and size. This metric can then be used to further assess the distribution of shape with populations of other fragment characteristics within these datasets. The shape parameterization using the L:D ratios of right-circular cylinders is discussed.
美国航天局的轨道碎片方案办公室依靠实验室撞击试验来补充确定轨道碎片环境的在轨事件测量数据。这些实验提供的信息对于将轨道碎片事件的雷达和光学测量结果解释为有用的指标(如特征尺寸)以及更好地了解碎片群在质量、材料成分、碎片密度、横截面积、面积与质量比、形状等方面的分布情况至关重要。卫星轨道碎片特征撞击试验是 1992 年利用美国海军 20 世纪 60 年代剩余的 Transit 导航卫星进行的一次引人注目的实验室撞击试验。这项地面实验的数据与在轨测量数据相结合,开发出了 NASA 标准卫星破裂模型(SSBM)。为了考虑到卫星设计和建造方面的进步,2014 年进行了新的撞击测试系列--DebriSat。该测试使用了高保真模拟航天器,更好地体现了设计和制造现代航天器所使用的材料和建造技术。这些测试为模拟由传统和现代航天器组成的轨道碎片环境提供了宝贵的数据。本文概述了这两项实验室撞击试验,比较了彼此的碎片参数分布以及美国航天局 SSBM 的相关分布。碎片形状的分类和描述对未来工作具有重要意义,但在形状类别的定义、组成材料的分类以及填充这两个数据集所采用的测量技术方面存在明显差异。新的标准简化并等同于数据集之间的分类,以帮助进行比较分析,并促进这两个数据集在未来环境碎片模型中的潜在使用。对不同数据集进行形状分类的首选方法是使用特征长度尺寸和基于物理实体尺寸的简化形状分类,以数学方法构建一个代表碎片的封装直圆柱体。圆柱体长度与直径之比(L:D)为形状提供了一个单一的连续值,该值与其指定的形状和尺寸密切相关。这一指标可用于进一步评估这些数据集中其他碎片特征的形状分布。本文讨论了使用直圆柱体的 L:D 比值进行形状参数化的方法。
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引用次数: 0
Investigation of near-rectilinear halo orbit search and rescue using staging L1/L2 Lyapunov and distant retrograde orbit families 利用分期 L1/L2 Lyapunov 和远距离逆行轨道族对近直角光环轨道搜索和救援的研究
Q3 ENGINEERING, AEROSPACE Pub Date : 2024-06-01 DOI: 10.1016/j.jsse.2024.04.009
Thomas J. Fay, Adam P. Wilmer, Robert A. Bettinger

Cislunar space is a region of growing interest with nations investing resources to cultivate long presence habitations on the lunar surface. With this increased attention and expansion of missions, both crewed and uncrewed, the likelihood of a mishap or a spacecraft becoming impaired and unable to continue its mission will also increase. The present research adds to the field of cislunar mission operations and trajectory analysis by investigating search and rescue (SAR) operations via rendezvous and proximity operations (RPO) with an impaired notional spacecraft located in a Near-Rectlinear Halo Orbit (NRHO). This research compares the response times of rescuer spacecraft located in sample distant retrograde orbits (DROs) and L1/L2 Lyapunov orbits for the timely far rendezvous with the impaired spacecraft located in the NRHO. This will simulate a variety of far rendezvous whereby the impaired spacecraft’s location within the NRHO and the rescuer spacecraft in the L1/L2 Lyapunov and DRO orbit families are varied. A series of minimum time optimal control problems are posed using the circular restricted three-body problem (CR3BP) dynamics, and pseudospectral methods are used to find solutions given an example maximum ΔV constraint of 3 km/s. The results reinforces our intuition that rendezvous time of flight (TOF) between orbits within the L1, L2, and DRO families and the targeted NRHO correlate with proximity to the NRHO, with the shortest far rendezvous times in each family found to be approximately 6 hours, 4.5 hours, and 10 hours respectively. The results further show that a constellation of two rescue spacecraft could be positioned within the three orbit families to achieve far rendezvous with the chosen NRHO in under one day.

随着各国投入资源在月球表面建立长期存在的居住地,人们对半月空间的兴趣与日俱增。随着关注度的增加以及载人和非载人飞行任务的扩大,发生事故或航天器受损而无法继续执行任务的可能性也会增加。本研究通过对位于近直角光环轨道(NRHO)的受损名义航天器进行交会和邻近操作(RPO)的搜救(SAR)行动进行调查,为半月形飞行任务操作和轨迹分析领域增添了新的内容。这项研究比较了位于样本远距离逆行轨道(DRO)和 L1/L2 Lyapunov 轨道上的救援航天器与位于 NRHO 上的受损航天器及时远距离会合的响应时间。这将模拟各种远距离会合,其中受损航天器在 NRHO 中的位置和救援航天器在 L1/L2 Lyapunov 和 DRO 轨道系列中的位置各不相同。利用环形受限三体问题(CR3BP)动力学提出了一系列最短时间最优控制问题,并使用伪谱法在最大 ΔV 约束为 3 公里/秒的示例条件下寻找解决方案。结果加强了我们的直觉,即 L1、L2 和 DRO 系列中的轨道与目标 NRHO 之间的会合飞行时间(TOF)与距离 NRHO 的远近相关,每个系列中最短的远距离会合时间分别约为 6 小时、4.5 小时和 10 小时。结果进一步表明,由两个救援航天器组成的星座可以在三个轨道系列内定位,以便在一天之内与选定的NRHO实现远距离会合。
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引用次数: 0
Commercial spaceflight: Regulatory framework assessment and safety perspectives 商业航天:监管框架评估和安全视角
Q3 ENGINEERING, AEROSPACE Pub Date : 2024-06-01 DOI: 10.1016/j.jsse.2024.04.004
G. Buzzo, L. Travascio, A. Vozella

Recent years are witnessing the rapid technological development in airspace domain, actually paving the way to the development of a commercial space market. Until the recent past, space operations have been essentially performed by research centers or military agencies, in usually segregated areas to ensure third parties’ safety, governed by launch base regulations and organized in an unscheduled manner. However, with the entry of private companies into the space domain, a new market niche is being created: that of commercial space transportation. For example, a promising area is the one related to operations performed by commercial suborbital flights, whether aimed at space tourism or simply transporting things and/or passengers from one point to another on the Earth's surface. The traffic volumes are supposed to increase in next years and segregating airspace does not represent a sustainable solution for the future.

The present paper will first assess the state of the art of the regulatory framework currently applicable to operators in order to obtain authorization to perform space missions for commercial use, then propose a comparison between the United State of America and European regulatory frameworks. Main challenges related to regulatory aspects will be identified and perspectives on possible higher airspace operations integration in the medium-long term will be derived. Finally, safety considerations deriving from a seamless accommodation of higher airspace operations in current Air Traffic Management will be derived for the medium-long term. In conclusion, this work reveals that neither the United States nor Europe has formally approved a legal framework establishing certification procedures for sub-orbital space transport systems. Currently, the US legislation is the most applicable as it has comprehensive rules to allow operators to obtain flight authorization ensuring compliance with requirements through a compliance matrix periodically updated.

近年来,空域领域的技术发展迅速,这实际上为商业空间市场的发展铺平了道路。直到最近,空间业务基本上都是由研究中心或军事机构进行的,通常是在隔离区内进行,以确保第三方的安全,受发射基地条例的制约,以非计划的方式组织。然而,随着私营公司进入太空领域,一个新的市场利基正在形成:商业太空运输。例如,一个很有前景的领域是商业亚轨道飞行的相关业务,无论是以太空旅游为目的,还是仅仅是将物品和/或乘客从地球表面的一个点运送到另一个点。本文件将首先评估目前适用于运营商的监管框架的最新情况,以便获得执行商业用途空间飞行任务的授权,然后对美国和欧洲的监管框架进行比较。将确定与监管方面有关的主要挑战,并对中长期内可能的更高空域运行一体化进行展望。最后,还将从中长期角度提出将高级空域运行无缝纳入当前空中交通管理的安全考虑因素。总之,这项工作表明,美国和欧洲都没有正式批准建立亚轨道空间运输系统认证程序的法律框架。目前,美国的立法最适用,因为它有全面的规则,允许运营商获得飞行授权,确保通过定期更新的合规矩阵符合要求。
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引用次数: 0
Antarctic station Vostok as an analogue of a future lunar base: physiological reactions of the human cardiorespiratory system during a year-long exposure to the conditions of hypobaric hypoxia, isolation and hypokinesia 作为未来月球基地模拟站的南极沃斯托克站:人体心肺系统在长达一年的低压氧、隔离和低运动状态下的生理反应
Q3 ENGINEERING, AEROSPACE Pub Date : 2024-06-01 DOI: 10.1016/j.jsse.2024.03.003
Nikolay Osetskiy, Olga Manko, Anton Artamonov, Eugeniy Ilyin , Oleg Orlov

A number of physiological investigations focused on human cardiorespiratory system have been conducted at Vostok station in Central Antarctica during the wintering of 2019.

During the one-year expedition at the Vostok station, the cardiorespiratory system gradually adapted to the unusual conditions of life and work in the isolated, confined and extreme (ICE) environment of Central Antarctica.

We hypothesized that during a long stay in the conditions of the Central Antarctica the adaptation strategy to physical environmental conditions for representatives of two age groups will differ, which will be evident from the dynamics of indicators of the functioning of the cardiovascular system and when assessing the autonomic nervous system status.

The level of blood oxygen saturation stabilized by the second month and was in the range of 86.0-91.0%, which corresponded to a reduced partial pressure of oxygen in the inhaled air. In terms of the respiratory system, central sleep apnea was noted in all subjects throughout the study. Quantitative analysis revealed that the average number of apneas per hour was 43, and their average duration was 25.2 seconds. The maximum apnea number was recorded at the beginning and middle of wintering, while before the end of the expedition the episodes became rarer. In all age groups there was a shortening of the PQ interval, with a tendency towards normalization by the end of wintering, while in the first age group the shortening of the interval was more significant than in the second, which apparently can be explained by a more pronounced active reaction of the sympathetic nervous system of polar explorers of the first age group.

Adaptive Potential Index (API) level remained practically unchanged throughout the wintering period in 9 out of 11 members of the expedition. The API value was predominantly in the range from 2.11 to 3.20 points, which corresponds to the level of “adaptation stress”. The autonomous nervous system (ANS) status was assessed by Kerdo Index (KI) values. KI positive dynamic was noted in 90% of cases by the 5th month of wintering. A direct correlation was found between the degree of positive shift in the KI value and the age of the participant. The gained results do not allow us to state that ANS has fully adapted to the conditions of life and work at the station. The results of this investigation demonstrate stable and positive adaptation trend to the ICE environment of Central Antarctica throughout the study period, regardless of age and wintering experience.

2019年越冬期间,在南极洲中部的沃斯托克站开展了一系列以人类心肺系统为重点的生理学调查。在沃斯托克站为期一年的考察期间,心肺系统逐渐适应了南极洲中部与世隔绝、封闭和极端(ICE)环境中不同寻常的生活和工作条件。我们假设,在南极洲中部长期居住期间,两个年龄组的代表对物理环境条件的适应策略将有所不同,这将从心血管系统功能指标的动态变化以及评估自律神经系统状态时显而易见。在呼吸系统方面,在整个研究过程中,所有受试者都出现了中枢性睡眠呼吸暂停。定量分析显示,每小时平均呼吸暂停次数为 43 次,平均持续时间为 25.2 秒。过冬初期和中期的呼吸暂停次数最多,而在探险结束前,呼吸暂停的次数则越来越少。在所有年龄组中,PQ 间期都有所缩短,到越冬结束时趋于正常,而在第一个年龄组中,PQ 间期的缩短比第二个年龄组更为明显,这显然可以解释为第一个年龄组的极地探险者的交感神经系统反应更为活跃。API 值主要在 2.11 至 3.20 点之间,相当于 "适应压力 "水平。自律神经系统(ANS)的状态是通过克度指数(KI)值来评估的。在越冬的第 5 个月,90% 的案例都出现了 KI 阳性动态。KI值的正向变化程度与参与者的年龄有直接关系。这些结果并不能说明 ANS 已经完全适应了车站的生活和工作条件。这项调查的结果表明,在整个研究期间,无论年龄和越冬经验如何,南极洲中部的冰川环境都呈现出稳定和积极的适应趋势。
{"title":"Antarctic station Vostok as an analogue of a future lunar base: physiological reactions of the human cardiorespiratory system during a year-long exposure to the conditions of hypobaric hypoxia, isolation and hypokinesia","authors":"Nikolay Osetskiy,&nbsp;Olga Manko,&nbsp;Anton Artamonov,&nbsp;Eugeniy Ilyin ,&nbsp;Oleg Orlov","doi":"10.1016/j.jsse.2024.03.003","DOIUrl":"10.1016/j.jsse.2024.03.003","url":null,"abstract":"<div><p>A number of physiological investigations focused on human cardiorespiratory system have been conducted at Vostok station in Central Antarctica during the wintering of 2019.</p><p>During the one-year expedition at the Vostok station, the cardiorespiratory system gradually adapted to the unusual conditions of life and work in the isolated, confined and extreme (ICE) environment of Central Antarctica.</p><p>We hypothesized that during a long stay in the conditions of the Central Antarctica the adaptation strategy to physical environmental conditions for representatives of two age groups will differ, which will be evident from the dynamics of indicators of the functioning of the cardiovascular system and when assessing the autonomic nervous system status.</p><p>The level of blood oxygen saturation stabilized by the second month and was in the range of 86.0-91.0%, which corresponded to a reduced partial pressure of oxygen in the inhaled air. In terms of the respiratory system, central sleep apnea was noted in all subjects throughout the study. Quantitative analysis revealed that the average number of apneas per hour was 43, and their average duration was 25.2 seconds. The maximum apnea number was recorded at the beginning and middle of wintering, while before the end of the expedition the episodes became rarer. In all age groups there was a shortening of the PQ interval, with a tendency towards normalization by the end of wintering, while in the first age group the shortening of the interval was more significant than in the second, which apparently can be explained by a more pronounced active reaction of the sympathetic nervous system of polar explorers of the first age group.</p><p>Adaptive Potential Index (API) level remained practically unchanged throughout the wintering period in 9 out of 11 members of the expedition. The API value was predominantly in the range from 2.11 to 3.20 points, which corresponds to the level of “adaptation stress”. The autonomous nervous system (ANS) status was assessed by Kerdo Index (KI) values. KI positive dynamic was noted in 90% of cases by the 5th month of wintering. A direct correlation was found between the degree of positive shift in the KI value and the age of the participant. The gained results do not allow us to state that ANS has fully adapted to the conditions of life and work at the station. The results of this investigation demonstrate stable and positive adaptation trend to the ICE environment of Central Antarctica throughout the study period, regardless of age and wintering experience.</p></div>","PeriodicalId":37283,"journal":{"name":"Journal of Space Safety Engineering","volume":"11 2","pages":"Pages 268-280"},"PeriodicalIF":0.0,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140784787","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
The planetary protection strategy of Mars Sample Return’s Earth Return Orbiter mission 火星取样返回地球轨道飞行器任务的行星保护战略
Q3 ENGINEERING, AEROSPACE 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

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.

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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Journal of Space Safety Engineering
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