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Garcia Perez, Andres ORCID: https://orcid.org/0000-0003-1444-9725, Chimeno Manguan, Marcos
ORCID: https://orcid.org/0000-0002-8290-8746, Sanz Andres, Angel Pedro
ORCID: https://orcid.org/0000-0001-5890-6065 and Alonso Rodrigo, Gustavo
ORCID: https://orcid.org/0000-0002-1220-5586
(2019).
Numerical results of modal coupling in the UPMSat-2 structure.
In: "8th European Conference For Aeronautics And Space Sciences (EUCASS)", 1-4 jul 2019, Madrid.
https://doi.org/10.13009/EUCASS2019-338.
Title: | Numerical results of modal coupling in the UPMSat-2 structure |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 8th European Conference For Aeronautics And Space Sciences (EUCASS) |
Event Dates: | 1-4 jul 2019 |
Event Location: | Madrid |
Title of Book: | EUCASS 2019 : 8th European Conference for Aeronautics and Space Sciences |
Date: | 2019 |
Subjects: | |
Faculty: | E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM) |
Department: | Aeronaves y Vehículos Espaciales |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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This work presents a study of the effects of modal coupling on the microsatellite UPMSat-2, where some design parameters are modified to achieve different levels of modal coupling. The finite element model (FEM) of the satellite is used to obtain the numerical results such as natural frequencies, interface forces and stresses resulted from the different configurations. The results show an appreciable reduction of the forces and stresses on the main structure when the degree of modal coupling is higher. However, the negative effect is the increase of the stresses on the secondary parts, which can overpass their allowable limits
Item ID: | 66878 |
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DC Identifier: | https://oa.upm.es/66878/ |
OAI Identifier: | oai:oa.upm.es:66878 |
DOI: | 10.13009/EUCASS2019-338 |
Official URL: | https://www.eucass.eu/2019/index.html |
Deposited by: | Memoria Investigacion |
Deposited on: | 19 Nov 2021 12:37 |
Last Modified: | 19 Nov 2021 12:37 |