Tesi etd-01132022-165410 |
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Tipo di tesi
Tesi di laurea magistrale
Autore
MAGNANTE, ENZO ROMAIN
URN
etd-01132022-165410
Titolo
Multi-Layer Insulation for Satellites - Design and Technology Improvement
Dipartimento
INGEGNERIA CIVILE E INDUSTRIALE
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Chiarelli, Mario Rosario
Parole chiave
- 3DEXPERIENCE
- quality control
- improvement
- design
- satellite
- multi-layer insulation
- grounding
- Digital Mock-Up
- mass budget
- export
- AIRBUS
- CATIA
- 3DX
- mli
Data inizio appello
15/02/2022
Consultabilità
Non consultabile
Data di rilascio
15/02/2092
Riassunto
6-months internship performed at Airbus Defence and Space in Toulouse (France). Missions related to the mechanical design of the Multi-Layer Insulation (MLI), thermal protections for satellites:
- Development of an automatic tool for quality control of MLI design on 3DEXPERIENCE (CATIA V6)
- Improvement of the export process towards manufacturers
- Improvement of the mass budget precision
- Improvement of the Digital Mock-Up (DMU) on 3DEXPERIENCE
- Development of a new electrical grounding technology compatible with Radio-Frequency issues
Due to confidentiality issue, this report is censored and contains only informations Airbus agreed to disclose. Thus, only my method is explained, and any details about technologies or results are described with code names.
This document and the information it contains are property of Airbus Defence and Space. It shall not be used for any purpose other than those for which it was supplied. It shall not be reproduced or disclosed (in whole or in part) to any third party without Airbus Defence and Space prior written consent. Airbus Defence and Space SAS – All rights reserved.
- Development of an automatic tool for quality control of MLI design on 3DEXPERIENCE (CATIA V6)
- Improvement of the export process towards manufacturers
- Improvement of the mass budget precision
- Improvement of the Digital Mock-Up (DMU) on 3DEXPERIENCE
- Development of a new electrical grounding technology compatible with Radio-Frequency issues
Due to confidentiality issue, this report is censored and contains only informations Airbus agreed to disclose. Thus, only my method is explained, and any details about technologies or results are described with code names.
This document and the information it contains are property of Airbus Defence and Space. It shall not be used for any purpose other than those for which it was supplied. It shall not be reproduced or disclosed (in whole or in part) to any third party without Airbus Defence and Space prior written consent. Airbus Defence and Space SAS – All rights reserved.
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