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Experimental and Numerical Assessment of Demisable Joints for Controlled Break-up of Large Sandwich Panel Structures

Ring, Alexander und Sakraker, Isil und Schleutker, Thorn (2026) Experimental and Numerical Assessment of Demisable Joints for Controlled Break-up of Large Sandwich Panel Structures. In: ESA Clean Space Days 2026. ESA Clean Space Days 2026, 2026-06-29 - 2026-07-03, Nordwijk, Niederlande.

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Kurzfassung

This work investigates the influence of demisable joints (DJs) on the atmospheric re-entry and ground-impact risk of the EarthCARE satellite using the SCARAB simulation framework. A high-fidelity reference model of the satellite was developed and adapted to incorporate demisable joints at selected primary structural interfaces. Different joint-triggering conditions and resulting structural separation scenarios were simulated to assess their effects on the re-entry process, breakup sequence, surviving debris mass, and Debris Casualty Area (DCA).

In parallel, bracket-type demisable joint samples developed at the German Aerospace Center (DLR) were successfully tested in a plasma wind tunnel (PWT). These tests provided an experimental assessment of the thermal response and demisability of the developed joint concept under representative re-entry heating conditions, complementing the numerical investigations.

In addition to evaluating the overall simulation results, a subsystem-level analysis methodology was developed to trace surviving fragments back to their subsystems of origin. This enables the quantification of absolute DCA changes for individual subsystems and provides insight into their respective contributions to ground-impact casualty risk. The approach supports the identification of critical structural interfaces and the assessment of different joint configurations and triggering conditions.

The results demonstrate the applicability of simulation-based analyses for investigating the potential benefits and limitations of demisable joints in satellite structures. However, the numerical findings are subject to the assumptions and limitations of the model and do not constitute experimental validation of joint functionality within the simulated EarthCARE configuration or a prediction of the actual satellite re-entry event. Further work should address the refinement of joint separation modelling, sensitivity to key simulation parameters, and integration of experimental test results to enable a more robust assessment of the potential of demisable joints to reduce surviving debris and associated ground-impact casualty risk.

elib-URL des Eintrags:https://elib.dlr.de/228649/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Experimental and Numerical Assessment of Demisable Joints for Controlled Break-up of Large Sandwich Panel Structures
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Ring, Alexanderalexander.ring (at) dlr.dehttps://orcid.org/0009-0003-4860-7821232206381
Sakraker, IsilIsil.Sakraker (at) dlr.dehttps://orcid.org/0000-0003-2666-3446232206382
Schleutker, ThornThorn.Schleutker (at) dlr.dehttps://orcid.org/0000-0002-1833-2850NICHT SPEZIFIZIERT
Datum:3 Juli 2026
Erschienen in:ESA Clean Space Days 2026
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Design for Demise, Demisable Joints, High-altitude break-up, Space Debris, Casualty Risk, Atmospheric Re-entry, Satellite Structures, Sandwich Panels, Zero Debris, Re-entry Analysis, SCARAB
Veranstaltungstitel:ESA Clean Space Days 2026
Veranstaltungsort:Nordwijk, Niederlande
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:29 Juni 2026
Veranstaltungsende:3 Juli 2026
Veranstalter :European Space Agency
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt Technologien für Mitigation von Space Debris [RP], R - Projekt Technologien für Mitigation von Space Debris [SY]
Standort: Stuttgart
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien
Institut für Bauweisen und Strukturtechnologie > Raumfahrt - System - Integration
Hinterlegt von: Ring, Alexander
Hinterlegt am:04 Nov 2026 13:37
Letzte Änderung:04 Nov 2026 13:37

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