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Improvement of the reliability and robustification of the Metal3D project, commissioned by ESA, the first metallic 3D printer to operate in orbit

Vincenzo Saladino

Improvement of the reliability and robustification of the Metal3D project, commissioned by ESA, the first metallic 3D printer to operate in orbit.

Rel. Marco Fioriti. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2024

Abstract:

The recent increase in space activities, particularly in Low Earth Orbit (LEO), brings significant attention to the issue of space sustainability, concerning the impact of these activities both on orbit and on Earth. One of the solutions identified by the scientific community is space additive manufacturing, which would allow for the recycling of space components already in orbit, that would otherwise become debris, as well as reducing the launch mass of satellites, thus optimizing the payload of space launch vehicles. A project led by the European Space Agency, called Metal3D, involving an industrial consortium headed by Airbus Defence and Space, aims to demonstrate the feasibility of using in-orbit additive manufacturing for the production of metallic parts. The technology demonstrator, which arrived on the International Space Station in 2024, has achieved this goal, although there is still significant room for improvement. This context frames the work presented in this Master Thesis: after an overview of the demonstrator’s hardware and software functioning, a series of improvements are presented, aimed at paving the way for the development of a more autonomous and efficient version of Metal3D. The proposed improvements range from the implementation of image processing and data fusion algorithms to enhance the in-situ monitoring process of printed parts, to the preliminary design of a closed-loop control system. The performance of each improvement is also evaluated through appropriate simulations, which demonstrate the interest and effectiveness of their future implementation in what will be Metal3D 2.0.

Relatori: Marco Fioriti
Anno accademico: 2024/25
Tipo di pubblicazione: Elettronica
Numero di pagine: 101
Informazioni aggiuntive: Tesi secretata. Fulltext non presente
Soggetti:
Corso di laurea: Corso di laurea magistrale in Ingegneria Aerospaziale
Classe di laurea: Nuovo ordinamento > Laurea magistrale > LM-20 - INGEGNERIA AEROSPAZIALE E ASTRONAUTICA
Ente in cotutela: ISAE-SUPAERO INSTITUT SUPERIEUR DE L'AERONAUTIQUE ET DE L'ESPACE (FRANCIA)
Aziende collaboratrici: Airbus Defence and Space
URI: http://webthesis.biblio.polito.it/id/eprint/33295
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