A review of satellite-based atomic oxygen sensing methods

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Progress in Aerospace Sciences Pub Date : 2023-02-01 DOI:10.1016/j.paerosci.2023.100886
Brandon E.A. Holmes, Vitor T.A. Oiko, Peter C.E. Roberts
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引用次数: 1

Abstract

The space industry has recently seen rising research interest in satellites developed to operate for extended periods at lower altitudes than ever before. The combination of lower launch costs, reduced radiation effects, and ease of deorbit, among other benefits, outlines very low Earth orbit (VLEO) missions as a key prospect of the space sector in the near future.

Neutral atomic oxygen (ATOX), the dominant gas species in lower orbital altitudes, is a major consideration for VLEO missions. The oxidising nature of ATOX with relative speeds at least 7.8 km/s can easily cause an early end to a satellite mission through generation of drag forces, as well as degradation of solar array surfaces and optical instruments. During a mission, accurate quantification of this erosion damage aboard the spacecraft may be gained though gathering data regarding ATOX gas flux impinging on susceptible surfaces at a given point in time.

Additionally, increased aerodynamic loading, caused by greater gas densities at lower altitudes, plays a substantial role in satellite station keeping and attitude control; an aerodynamically unstable spacecraft may experience undesirable rotational forces or even enter a tumbling state if left unchecked. Real-time measurement of ATOX flux allows a mission to determine short-term variations in ATOX flux and therefore estimate fluctuations of satellite lift and drag, enabling a satellite to react appropriately. Long-term recording of these fluctuations may also hold influence over future satellite aerodynamic design.

Atomic oxygen sensing methods are a crucial aspect of future VLEO satellite design as we begin to tackle the obstacles of reduced altitude orbits. These sensors are able to measure the quantity of atomic oxygen atoms impinging on a satellite per unit area. In the interest of reacting to, and designing for the erosive environment and aerodynamic forces presented by ATOX and gas species in VLEO, we review available ATOX sensing methods and their respective applications.

Each ATOX sensing method has its own benefits and drawbacks. The most appropriate method for a given mission depends on factors such as altitude, mission lifetime, and mass budget. A review of the most common methods will clarify design options, and outline suitable areas for future research.

This paper builds upon a review of ATOX measurement methods performed by Osborne, et al. in 2001, updating with technologies from the past two decades as well as providing further examples of each method’s real-world applications.

It also conducts a semiquantitative analysis of spacecraft-based atomic oxygen sensing methods, describing the relative merits of each and their relevant applications. Generalised recommendations are made with regards to the most appropriate sensing method for a range of satellite mission scenarios.

This review finds that proven methods, such as mass spectroscopy, remain the most appropriate sensing methods for many missions. However, the progress seen within technologies of lower heritage, such as renewable actinometers, suggests that we may see missions exhibiting more recent ATOX sensing methods in the near future.

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卫星原子氧传感方法综述
航天工业最近对开发出的能够在比以往任何时候都低的高度长时间运行的卫星的研究兴趣越来越高。较低的发射成本、减少的辐射影响和易于脱轨等优点,使极低地球轨道(VLEO)任务成为近期太空领域的一个关键前景。中性原子氧(ATOX)是低轨道高度的主要气体物种,是VLEO任务的主要考虑因素。ATOX的氧化性质相对速度至少为7.8公里/秒,通过产生阻力以及太阳能电池阵列表面和光学仪器的退化,很容易导致卫星任务提前结束。在执行任务期间,通过收集在给定时间点撞击易感表面的ATOX气体流量的数据,可以获得航天器上这种侵蚀损伤的准确量化。此外,由于在较低高度气体密度较大,空气动力学载荷增加,在卫星站保持和姿态控制方面发挥了重要作用;如果不加以控制,空气动力学不稳定的航天器可能会经历不希望的旋转力,甚至进入翻滚状态。通过实时测量ATOX通量,任务可以确定ATOX通量的短期变化,从而估计卫星升力和阻力的波动,使卫星能够做出适当的反应。这些波动的长期记录也可能对未来的卫星空气动力学设计产生影响。随着我们开始解决低空轨道的障碍,原子氧传感方法是未来VLEO卫星设计的一个关键方面。这些传感器能够测量每单位面积撞击卫星的原子氧原子的数量。为了对ATOX和VLEO中的气体物种所呈现的侵蚀环境和空气动力做出反应和设计,我们回顾了可用的ATOX传感方法及其各自的应用。每种ATOX传感方法都有其自身的优点和缺点。对于给定的任务,最合适的方法取决于海拔、任务寿命和质量预算等因素。对最常见方法的审查将澄清设计选项,并概述未来研究的合适领域。本文建立在Osborne等人2001年对ATOX测量方法的回顾之上,用过去二十年的技术进行了更新,并提供了每种方法在现实世界中应用的进一步例子。它还对基于航天器的原子氧传感方法进行了半定量分析,描述了每种方法的相对优点及其相关应用。就一系列卫星任务场景中最合适的传感方法提出了一般性建议。这篇综述发现,经过验证的方法,如质谱法,仍然是许多任务中最合适的传感方法。然而,可再生光量计等低传统技术的进展表明,在不久的将来,我们可能会看到任务展示出更新的ATOX传感方法。
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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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