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

Development of a Testbed for the Beneficiation of Lunar Regolith - Concentrating an Ilmenite-Rich Feedstock for In-Situ Oxygen Production on the Moon

Franke, Michel Fabien (2022) Development of a Testbed for the Beneficiation of Lunar Regolith - Concentrating an Ilmenite-Rich Feedstock for In-Situ Oxygen Production on the Moon. Masterarbeit, Universität Bremen.

[img] PDF
10MB

Kurzfassung

The utilization of extraterrestrial resources may one day enable mankind’s further exploration and sustainable colonization of the Solar System. An easily accessible and very versatile resource found on Earth’s celestial neighbor, the Moon, is lunar regolith. This unconsolidated mixture of soil and rocks contains large quantities of oxygen, which in return can be used to produce consumables for propulsion and life support systems. However, the oxygen is chemically bound to minerals and must, thus, be extracted. The preparation of a feedstock that is chemically and physically suited for the extraction is termed beneficiation and depicts a vital stage in the context of in-situ oxygen production. Developing a test stand that demonstrates the technical feasibility of lunar mineral beneficiation in a laboratory setting is the purpose of this master’s thesis. The testbed’s main function is to concentrate the target mineral ilmenite (a titanium-iron oxide), to reject unwanted gangue minerals (like silicates), and to remove unfavored size fractions (e.g., dedusting and oversize grain removal). To ensure that the end product fulfills this function in a satisfactory manner, a systematic engineering design process consisting of seven work packages is applied. This involves a review of existing studies and an investigation of available processes, the definition of requirements and specification, as well as various conceptualization activities (process and setup selection plus sketching). Moreover, results of design calculations and data of methodically selected components are integrated into a 3D model, to be created using computer-aided design software. Production planning activities like the preparation of procurement-related documentation completes the development. The outcome of this thesis is a well-engineered and methodically mature beneficiation system that encompasses three dry separation stages: Particle size separation, magnetic separation, and electrostatic separation. This multi-stage approach guarantees the reliable and efficient enrichment of ilmenite from lunar regolith simulant. Hence, it is ready to be brought into being through assembly, integration, and test and can eventually be used for beneficiation-related experiments.

elib-URL des Eintrags:https://elib.dlr.de/185548/
Dokumentart:Hochschulschrift (Masterarbeit)
Titel:Development of a Testbed for the Beneficiation of Lunar Regolith - Concentrating an Ilmenite-Rich Feedstock for In-Situ Oxygen Production on the Moon
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Franke, Michel Fabienmichel.franke (at) dlr.dehttps://orcid.org/0000-0002-7722-7946NICHT SPEZIFIZIERT
Datum:2022
Referierte Publikation:Nein
Open Access:Ja
Status:veröffentlicht
Stichwörter:In-situ resource utilization (ISRU), Space resource utilization (SRU), Extraterrestrial oxygen production, Lunar mineral beneficiation, Mineral enrichment of ilmenite
Institution:Universität Bremen
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 - CEF Studien
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Systemanalyse Raumsegment
Hinterlegt von: Zabel, Paul
Hinterlegt am:08 Mär 2022 09:40
Letzte Änderung:10 Okt 2024 09:39

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

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