2022
Journal article  Open Access

The Kinetic casualty risk of uncontrolled re-entries before and after the transition to small satellites and mega-constellations

Pardini C., Anselmo L.

Uncontrolled re-entries  Casualty expectancy  Casualty probability  Re-entry risk evaluation  Kinetic casualty risk  Risk  Aerospace Engineering  Safety  Reliability and Quality  Casualty area 

Over the last 11 years (2010-2020), more than 600 intact objects larger than 1 m^2 have re-entered without control into the Earth's atmosphere. The total returned mass was approximately 1100 t, roughly corresponding to the re-entry of nearly 100 t per year, mostly concentrated (79%) in rocket bodies. Objects with a mass greater than 500 kg re-entered every about 8 days, those exceeding 2000 kg every about 2 weeks and those heavier than 5000 kg one or twice per year. The total casualty expectancy associated with uncontrolled re-entries over the past 11 years was of the order of 1.4 × 10^-1, that in 2020 was almost 1.7 × 10^-2, corresponding to a probability of having had at least one victim of approximately 13% and 2%, respectively. Unlike the alert threshold of 10^-4, linked to single re-entry events, no cumulative risk limit exists for satellite re-entries over one year or more. However, the casualty probability, although still relatively small, cannot be considered negligible, even in view of the launches of mega-constellations planned in the coming years. For instance, if no design for demise was implemented, the addition of 4000 spacecraft re-entering annually would increase the probability of having at least one victim to nearly 30% per year, while 20,000 more satellites would boost it to almost 80%.

Source: Journal of Space Safety Engineering 9 (2022): 414–426. doi:10.1016/j.jsse.2022.04.003

Publisher: Elsevier


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BibTeX entry
@article{oai:it.cnr:prodotti:470380,
	title = {The Kinetic casualty risk of uncontrolled re-entries before and after the transition to small satellites and mega-constellations},
	author = {Pardini C. and Anselmo L.},
	publisher = {Elsevier},
	doi = {10.1016/j.jsse.2022.04.003},
	journal = {Journal of Space Safety Engineering},
	volume = {9},
	pages = {414–426},
	year = {2022}
}