elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Barrierefreiheit | Kontakt | English
Schriftgröße: [-] Text [+]

Evaluating End-of-Life Scenarios for Satellites Using Life Cycle Assessment

Koffler, Joséphine und Lampariello, Roberto und Albano, Joana und Pohya, Ahmad Ali und Rahn, Antonia und Wende, Gerko (2025) Evaluating End-of-Life Scenarios for Satellites Using Life Cycle Assessment. In: Proceedings of the 11th European Conference for AeroSpace Sciences (EUCASS 2025). EUCASS association. 11th EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS), 2025-06-30 - 2025-07-04, Rome, Italy. doi: 10.13009/EUCASS2025-203.

[img] PDF
1MB

Offizielle URL: https://www.eucass.eu/component/docindexer/?task=download&id=7612

Kurzfassung

As the number of satellites in orbit continues to grow, the end-of-life (EoL) phase of spacecraft presents critical challenges for orbital sustainability and environmental responsibility. Current EoL strategies, such as natural reentry, controlled reentry, and graveyard orbits, aim to mitigate space debris but have varying environmental implications that remain insufficiently explored. During reentry, up to 90% of satellites are vaporized [11], releasing metals, resins, and other toxic substances into the atmosphere [7], contributing to acidification, climate change, and particulate matter formation. Graveyard orbits, while reducing short-term collision risks, exacerbate long-term orbital congestion, and fragmentation potential. This study addresses the current methodological gap in environmental assessments of satellite EoL scenarios by introducing a combined Life Cycle Assessment (LCA) framework that integrates the Environmental Footprint 3.1 method with a dedicated Space Debris Indicator (SDI), enabling the evaluation of both terrestrial and orbital impacts. This combined framework evaluates environmental trade-offs across terrestrial, atmospheric, and orbital environments, providing an integrated view of satellite EoL impacts. Using a CubeSat as a case study, results indicate that controlled reentry has a higher environmental burden than natural reentry across multiple impact categories, not only due to fuel combustion but also because of a higher percentage of material ablation [13]. While natural reentry generates relatively lower atmospheric emissions, it results in a larger mass of surviving fragments. However, these fragments contribute minimally to the overall environmental impact compared to the emissions from atmospheric ablation. In contrast, graveyard orbits eliminate atmospheric emissions entirely but represent the most significant challenge for long-term orbital sustainability, with the highest Space Debris Index, underscoring their lasting impact on orbital congestion and fragmentation risks. These findings underscore the need for EoL strategies that balance short-term environmental impacts with long-term orbital sustainability. Exploring circular economy principles and innovative materials, such as wood-based structures to mitigate aluminum oxide pollution, presents promising pathways. Additionally, enhancing on-orbit operations through maintenance, repair, and upgrading would extend satellite lifespans, possibly reduce new launches and support orbital sustainability goals.

elib-URL des Eintrags:https://elib.dlr.de/219144/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Evaluating End-of-Life Scenarios for Satellites Using Life Cycle Assessment
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Koffler, Joséphinejosephine.koffler (at) dlr.dehttps://orcid.org/0009-0001-9263-3790197601220
Lampariello, RobertoRoberto.Lampariello (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Albano, Joanajoana.albano (at) dlr.dehttps://orcid.org/0009-0004-0809-3691197601222
Pohya, Ahmad AliAhmad.Pohya (at) dlr.dehttps://orcid.org/0000-0002-2734-3199NICHT SPEZIFIZIERT
Rahn, AntoniaAntonia.Rahn (at) dlr.dehttps://orcid.org/0000-0002-0528-5629NICHT SPEZIFIZIERT
Wende, Gerkogerko.wende (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2025
Erschienen in:Proceedings of the 11th European Conference for AeroSpace Sciences (EUCASS 2025)
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.13009/EUCASS2025-203
Verlag:EUCASS association
Status:veröffentlicht
Stichwörter:Satellite, End-of-life, Life cycle assessment
Veranstaltungstitel:11th EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS)
Veranstaltungsort:Rome, Italy
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:30 Juni 2025
Veranstaltungsende:4 Juli 2025
Veranstalter :European Conference for AeroSpace Sciences
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Robotik
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RO - Robotik
DLR - Teilgebiet (Projekt, Vorhaben):R - Impulsprojekt Orbitale Nachhaltigkeit [RO]
Standort: Hamburg
Institute & Einrichtungen:Institut für Instandhaltung und Modifikation
Institut für Robotik und Mechatronik (ab 2013)
Hinterlegt von: Koffler, Josephine
Hinterlegt am:21 Nov 2025 22:07
Letzte Änderung:21 Nov 2025 22:07

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
OpenAIRE Validator logo electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.