A new impact assessment model to integrate space debris within the life cycle assessment-based environmental footprint of space systems

Thibaut Maury-Micolier, Alice Maury-Micolier, A. Hélias, G. Sonnemann, P. Loubet
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引用次数: 2

Abstract

By analogy to conventional environmental impacts, the potential release of debris or generation of fragments can be considered as the emission of an environmental stressor damaging the orbital ‘natural’ resource which supports space activities. Hence, it appears relevant to integrate systematically the impact of the emission of debris on the orbital resource within the life cycle impact assessment (LCIA) step to broaden the scope of life cycle assessment (LCA) for space systems. The main objective of this article is to propose a set of characterization factors to compute the impact caused by the generation of debris within the orbital environment. To do so, the proposed approach follows the methodology of emission-related characterization models in LCIA. the characterization model enables to link the emission of debris and final economic damages to space activities through a complete impact pathway including the fate of debris in downstream orbital compartments, the exposure of targeted space objects to this debris, and the economic damage in case of collision between the debris and the space object. The model is computed for different compartments of the low earth orbit (LEO) region thanks to a discretization of the orbital environment. Results show that the potential damages are the highest for orbital compartments located in the orbital bands of altitude/inclination: 550–2000 km/52–54°, 1,200–2000 km/86–88°, 400–2000 km/96–100°, because of the downstream location of Starlink constellation, OneWeb constellation, and earth observation satellites, respectively. The proposed set of CFs can be used in the LCA of different space systems in order to include impacts and damages related to space debris, along with other environmental impacts. This original development fully in line with the standardized LCIA framework would have potential for further integration into harmonised sector-specific rules for the European space sector such as product environmental footprint category rules (PEFCR).
将空间碎片纳入基于生命周期评估的空间系统环境足迹影响评估新模型
与传统的环境影响类似,碎片的潜在释放或碎片的产生可被视为环境压力源的释放,破坏支持空间活动的轨道“自然”资源。因此,有必要在生命周期影响评估(LCIA)步骤中系统地整合碎片发射对轨道资源的影响,以扩大空间系统生命周期评估(LCA)的范围。本文的主要目的是提出一套表征因子来计算轨道环境中碎片产生所造成的影响。为此,提出的方法遵循LCIA中与排放相关的表征模型的方法。表征模型能够通过完整的撞击路径将碎片的排放和最终经济损失与空间活动联系起来,包括下游轨道舱内碎片的命运、目标空间物体对这些碎片的暴露以及碎片与空间物体碰撞时的经济损失。利用轨道环境的离散化,对低地球轨道区域的不同舱室进行了模型计算。结果表明:由于星链星座、OneWeb星座和对地观测卫星分别位于轨道高度/倾角550 ~ 2000 km/52 ~ 54°、1200 ~ 2000 km/86 ~ 88°和400 ~ 2000 km/96 ~ 100°的下游位置,轨道舱室的潜在损害最大;拟议的一套综合风险因素可用于不同空间系统的生命周期分析,以便包括与空间碎片有关的影响和损害以及其他环境影响。这一完全符合标准化LCIA框架的原始发展将有可能进一步整合到欧洲空间部门的协调部门特定规则中,例如产品环境足迹类别规则(PEFCR)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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