2021
DOI: 10.1016/j.actaastro.2020.09.034
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Re-entry survival analysis and ground risk assessment of space debris considering by-products generation

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Cited by 28 publications
(14 citation statements)
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“…Even the Falcon 9 reusable first stage rocket only reserves ∼6% of total fuel mass for controlled re‐entry and landing (Kim et al., 2021 ). Re‐entry heating NO x emissions from returning crewed spacecraft and rocket components should be parameterized using re‐entry velocity, trajectory, surface area and mass (Park et al., 2021 ), but only mass is readily available. We determine NO x emissions equivalent to 17.5% of the mass of each returning reusable component.…”
Section: Methodsmentioning
confidence: 99%
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“…Even the Falcon 9 reusable first stage rocket only reserves ∼6% of total fuel mass for controlled re‐entry and landing (Kim et al., 2021 ). Re‐entry heating NO x emissions from returning crewed spacecraft and rocket components should be parameterized using re‐entry velocity, trajectory, surface area and mass (Park et al., 2021 ), but only mass is readily available. We determine NO x emissions equivalent to 17.5% of the mass of each returning reusable component.…”
Section: Methodsmentioning
confidence: 99%
“…We model complete vapourization of rocket stages discarded above 50 km during launch, controlled payload re‐entries and unplanned re‐entry of space debris, resulting in NO x emissions equivalent to 100% of the mass of the re‐entering object. Additional organic and inorganic pollutants form due to the complex range of chemical matrices of rocket propellants and parts and extreme temperatures during both launch and re‐entry (Park et al., 2021 ), but there are only reported emission factors for the most common air pollutants (chlorine, BC, H 2 O, Al 2 O 3 and NO x ).…”
Section: Methodsmentioning
confidence: 99%
“…To mitigate this threat, recent attention has been paid to reducing the risk and controlling space debris and space junk in orbit (Maclay & McKnight, 2021;Madi & Sokolova, 2020;Unfried & Eder, 2021). Further, recent studies aim to quantify and provide a means for accurately communicating risks and hazards of space debris on the ground (Park et al, 2021). Byers et al (2022) study on abandoned rocket bodies reflects the growing likelihood of human casualty in the near future and the disproportionate risk imposed upon populations in the Global South which tend to receive more falling debris than the Global North.…”
Section: Theoretical Framework and Literature Reviewmentioning
confidence: 99%
“…Even the Falcon 9 reusable first stage rocket only reserves ∼6% of total fuel mass for controlled re-entry and landing (Kim et al, 2021). Re-entry heating NO x emissions from returning crewed spacecraft and rocket components should be parameterized using re-entry velocity, trajectory, surface area and mass (Park et al, 2021), but only mass is readily available. We determine NO x emissions equivalent to 17.5% of the mass of each returning reusable component.…”
Section: Emission Inventory Developmentmentioning
confidence: 99%
“…We model complete vapourization of rocket stages discarded above 50 km during launch, controlled payload re-entries and unplanned re-entry of space debris, resulting in NO x emissions equivalent to 100% of the mass of the re-entering object. Additional organic and inorganic pollutants form due to the complex range of chemical matrices of rocket propellants and parts and extreme temperatures during both launch and re-entry (Park et al, 2021), but there are only reported emission factors for the most common air pollutants (chlo rine, BC, H 2 O, Al 2 O 3 and NO x ).…”
Section: Emission Inventory Developmentmentioning
confidence: 99%