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Concept and Analysis of a Passive, Ballistic Re-entry Capsule for Sample Return Missions

Springer, Ole (2025) Concept and Analysis of a Passive, Ballistic Re-entry Capsule for Sample Return Missions. Masterarbeit, University of Bremen.

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Kurzfassung

This Master's thesis presents the concept and analysis of a passive, ballistic re-entry capsule for the return of collected samples. The proposed capsule is designed to transport approximately one litre of material without relying on active systems during entry, descent, and landing. The study evaluates various system configurations, including structural design, thermal protection, and impact dynamics, with particular emphasis on minimizing shocks to the sample container. A literature review of existing and planned sample return missions, along with potential design options, provides context for the conceptual design process. Numerical analyses are used to investigate possible re-entry trajectories and quantify the resulting mechanical and thermal loads. Based on these results, a thermal analysis estimates the necessary heat shield requirements, while structural simulations assess the capsule's integrity during re-entry. An impact analysis based on LS-DYNA determines the required dimensions of the energy-absorbing material to ensure sufficient shock attenuation during landing. The findings confirm the feasibility of the passive capsule concept and identify its operational limits. This work offers a foundation for future design iterations and positions the concept as a promising candidate for a reliable, lightweight, and versatile capsule for sample return missions.

elib-URL des Eintrags:https://elib.dlr.de/215823/
Dokumentart:Hochschulschrift (Masterarbeit)
Titel:Concept and Analysis of a Passive, Ballistic Re-entry Capsule for Sample Return Missions
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Springer, Oleole.springer (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
DLR-Supervisor:
BeitragsartDLR-SupervisorInstitution oder E-Mail-AdresseDLR-Supervisor-ORCID-iD
Thesis advisorRittweger, Andreasandreas.rittweger (at) dlr.dehttps://orcid.org/0000-0002-8398-0467
Thesis advisorSchneider, AntonAnton.Schneider (at) dlr.dehttps://orcid.org/0000-0003-4542-6251
Datum:2025
Open Access:Nein
Status:veröffentlicht
Stichwörter:Entry, Descent, Landing, Touchdown, Entry Probe, Sample Return
Institution:University of Bremen
Abteilung:Faculty of Production Engineering
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Technik für Raumfahrtsysteme
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R SY - Technik für Raumfahrtsysteme
DLR - Teilgebiet (Projekt, Vorhaben):R - Entfaltbarer Lande- und Rückkehrdemonstrator
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Land und Explorationstechnologie
Hinterlegt von: Schneider, Anton
Hinterlegt am:14 Aug 2025 09:13
Letzte Änderung:14 Aug 2025 09:13

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