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Satellite density distribution in LEO with the Starlink and OneWeb mega-constellations as filed (and amended) with the FCC. Provided that the orbits are nearly circular, the number densities in those shells will exceed 10–6 km⁻³. Because the collisional cross-section in those shells is also high, they represent regions that have a high collision risk whenever debris is too small to be tracked or collision avoidance manoeuvres are impossible for other reasons.

Satellite density distribution in LEO with the Starlink and OneWeb mega-constellations as filed (and amended) with the FCC. Provided that the orbits are nearly circular, the number densities in those shells will exceed 10–6 km⁻³. Because the collisional cross-section in those shells is also high, they represent regions that have a high collision risk whenever debris is too small to be tracked or collision avoidance manoeuvres are impossible for other reasons.

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The rapid development of mega-constellations risks multiple tragedies of the commons, including tragedies to ground-based astronomy, Earth orbit, and Earth’s upper atmosphere. Moreover, the connections between the Earth and space environments are inadequately taken into account by the adoption of a consumer electronic model applied to space assets....

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... There is very little data on the environmental impact of deorbiting on atmospheric chemistry and in-situ data collection is practically impossible. The few existing studies agree that while the current impact of deorbiting is likely negligible, the projected exponential growth of satellites in LEO (Ciocca et al., 2021) and the ensuing need to deorbit these objects could exacerbate the risks of damaging the ozone layer (Pultarova, 2021), as well as lead to a runaway, uncontrolled solar radiation management experiment on a planetary scale (Boley and Byers, 2021). While there are currently around 9000 satellites in orbit (ESA 2023b), the United Nations Office for Outer Space Affairs (UNOOSA, 2023a) reports that '35 per cent of all satellites launched over the past three years' (p. 3) and that there is the potential of 100,000 satellites being launched over the next decade. ...
... Both studies find 'that the atmospheric impact of spacecraft reentries is relatively low, there are still high-level uncertainties on aerothermodynamics and atmospheric chemistry-transport modelling and a lack of observational (in-situ) data to evaluate assumptions and models' (ESA, 2022). Some other studies conclude that '[t]he predicted strong increase in anthropogenic injection [of deorbited space derbis] will make it significant in comparison to the natural injection [meteoroids] which can have yet unknown effects on Earth's atmosphere and the terrestrial habitat' (Schulz and Glassmeier, 2021), that satellites could soon become the dominant source of high-altitude alumina (Boley and Byers, 2021), and that 'radiative forcing from space debris aluminium, interactions with high altitude cloud formation and possible consequences on measurement techniques of the middle atmosphere appear to be feasible consequences of space debris re-entries' (Jain and Hastings, 2022). Recently, a study by Murphy et al. (2023) revealed that '[a]bout 10% of stratospheric sulfuric acid particles larger than 120 nm in diameter contain aluminium and other elements from spacecraft reentry'. ...
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Space debris is a major issue for space safety as any collision of a space object with even a small piece of debris can have catastrophic consequences. The most recent dramatic increase of the number of satellites in Earth’s orbit is clearly exacerbating the risks. In this context there is a growing norm of disposal of orbital debris through atmospheric re-entry: space debris is to ‘burn up harmlessly in the atmosphere’, in order to provide for a ‘clean space’. Unfortunately, there is very little data on the environmental impact of deorbiting on atmospheric chemistry and in-situ data collection is practically impossible. The few existing studies – our own modelling included – agree that while the current impact of deorbiting is likely negligible, the projected exponential growth of satellites in LEO could exacerbate the risks. In consequence, space sustainability may come at the expense of damaging the health of the middle and upper atmosphere, with potentially unforeseeable consequences. Against this backdrop, we argue that in order to manage LEO sustainably, we must overcome this – what we call – ‘atmosphere-blindness’: our limited understanding of space-Earth system links through orbital disposal practices and their atmospheric impacts. While there is growing environmental consciousness with regard to outer space, we need to acknowledge that space sustainability is embedded in a wider context of outer space geopolitics, where the benefits and risks of the space infrastructure are distributed highly unequally. In our view it is thus crucially important to undertake more interdisciplinary research on the issue of de-orbiting, as it is not merely a technical environmental problem to be fixed but also an inherently political matter of planetary scale environmental justice.
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... The syndrome predicts the denial of protected space regions through space debris build-up and its onset can already be observed in Fig. 1. However, recent trends have intensified the problem as thousands of satellites are launched to form mega-constellations in LEO [4]. ...
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As artificial objects in Low Earth Orbit (LEO) become more numerous, the risk for breakup events threatening space-based services increases rapidly. Laser ablation methods have previously been proposed for the removal of small-size (1 - 10 cm) debris fragments, but a mission-level feasibility study is yet to be performed. This work investigates the mission concept and spacecraft design feasibility of a space-based laser aiming to de-orbit 50% of the debris generated by an on-orbit catastrophic event, using an agent-based modelling approach applied to the 2009 Cosmos-Iridium collision example. Several parameters were varied to generate a feasibility envelope on the payload performance, showing that the necessary capabilities for mission feasibility are within ranges achievable with current or near-term technology. Additionally, the financial challenges of the mission are discussed. A cost estimate for a single-flight mission of 550 M€ was generated based on the conceptual design developed for this study and is in agreement with previous research. This work shows that a laser ablation concept for the removal of small-size debris in LEO is feasible both technically and financially. It further provides a modelling base for future research on similar concepts for different mission scenarios.
... Resident space objects refer to both active and inactive satellites, spacecraft, debris or any human-made object in space. The number of satellites being launched into orbit is rapidly increasing due to mega constellations developed by companies including SpaceX, OneWeb, Amazon, Telesat and GW [8]. Space debris in particular poses a significant risk to the operation of global positioning systems, telecommunications and weather forecasting because the debris can deorbit, explode or cause collisions creating even more debris [9]. ...
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The large quantity of resident space objects orbiting Earth poses a threat to safety and efficient operations in space. Radar sensors are well suited to detecting objects in space including decommissioned satellites and debris, whereas the more commonly used optical sensors are limited by daylight and weather conditions. Observations of three non-operational satellites using a VHF radar system are presented in this paper in the form of micro Doppler signatures associated with rotational motion. Micro Doppler signatures are particularly useful for characterising resident space objects at VHF given the limited bandwidth resulting in poor range resolution. Electromagnetic simulations of the micro Doppler signatures of the defunct satellites are also presented using simple computer-aided design (CAD) models to assist with interpretation of the radar observations. The simulated micro Doppler results are verified using the VHF radar data and provide insight into the attitude and spin axis of the three resident space objects. As future work, this approach will be extended to a larger number of resident space objects which requires a automated processing.
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Conference Paper
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... The key policy issues to consider range from spectrum allocation and coordination (especially as 6G shifts to more of a 3D network structure) (Polese et al., 2023b), through to collision and space debris risks for drones and mega-constellations. Environmental impact assessment will also be important to avoid negative environmental externalities, including light pollution and emissions (Boley and Byers, 2021;Guyot et al., 2023;Osoro et al., 2023;Wilson, 2022). ...
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... There is increasing interest in space domain awareness (SDA) worldwide due to the increasing number of resident space objects (RSOs) [1]. This number has expanded rapidly in recent years due to the advent of mega-constellations such as the SpaceX Starlink constellation [2]. ...
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... The CW model has been exploited for numerous rendezvous and formation flying applications [18][19][20][21][22][23][24][25] in circular orbits in near-Earth space, and subsequently used for modeling orbital dynamics in this work. Furthermore, the application of the CW equations is suitable for a large number of artificial objects in nearly circular LEOs [26]. The CW equations accommodate additional control variables that enable us to describe the dynamics of controllable objects, such as active satellites, and non-controllable objects, such as defunct satellites and debris. ...
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... The uncontrolled re-entry of thousands of satellites into Earth's atmosphere could also pose a hazard to people and property on the ground and to airplanes in flight 2 . Re-entries could also alter Earth's upper atmosphere chemistry in non-trivial ways, owing to ablation products that are wildly different from the background flux of meteoroids [3][4][5] . ...
... Satellite re-entries from mega-constellations are likely to become the dominant source of high-altitude alumina in the near future, with presently unknown effects. 175 The prediction of nitric oxide due to entering debris or re-useable components is relatively easy as the high temperature air chemistry is well understood. On the contrary, the effect and amount of soot and black carbon emissions are principally unknown, and no validated predictive tools exist. ...
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