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1. Identity statement
Reference TypeConference Paper (Conference Proceedings)
Sitemtc-m21b.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W34P/3L9L7TS
Repositorysid.inpe.br/mtc-m21b/2016/03.03.14.19
Metadata Repositorysid.inpe.br/mtc-m21b/2016/03.03.14.19.39
Metadata Last Update2021:02.11.18.20.02 (UTC) administrator
Secondary KeyINPE--PRE/
Citation KeyMarquesDSMSFPCMMMDCMS:2016:MoAn3D
TitleStudy of rigid structure vibrations and mechanical modeling for the NANOSATC-BR2: modal analysis and 3D printing considerations
Year2016
Access Date2024, May 18
Secondary TypePRE CI
2. Context
Author 1 Marques, Rodrigo Passos
 2 Dutra, Viktor Bizarro
 3 Slongo, Artur Gustavo
 4 Mantovani, Lorenzo Quevedo
 5 Santos, Thaffarel
 6 Farias, Tiago
 7 Piovesan, Tális
 8 Costa, Leonardo Zavareze da
 9 Moro, Pietro Fernando
10 Mânica, Thales Ramos
11 Müller, Alex
12 Durão, Otávio Santos Cupertino
13 Caetano, Nattan Roberto
14 Machado, Renato
15 Schuch, Nelson Jorge
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12 8JMKD3MGP5W/3C9JJ2L
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12 DMC-ETE-INPE-MCTI-GOV-BR
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Affiliation 1 Instituto Nacional de Pesquisas Espaciais (INPE)
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 3 Instituto Nacional de Pesquisas Espaciais (INPE)
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 8 Instituto Nacional de Pesquisas Espaciais (INPE)
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12 otavio.durao@inpe.br
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Conference NameLatin American IAA CubeSat Workshop, 2
Conference LocationFlorianópolis, SC
Date28 Feb. - 02 Mar.
History (UTC)2016-03-03 14:19:39 :: simone -> administrator ::
2021-02-11 18:20:02 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
AbstractThe main purposes of this paper are to introduce a Rigid Structure Vi-bration Analysis for the NANOSATC-BR2 - 2U CubeSat - combining data that was calculated and tested on the NANOSATC-BR1 - 1U Cu-beSat - (tests carried out at LIT/INPE-MCTI), and show the results of the process of mechanical modeling for the NANOSATC-BR2, made with the Computer Aided Design (CAD) software Solidworks. In order to set parameters for the calculations to the Modal Analysis, a computa-tional model of the 2U CubeSat - NANOSATC-BR2 is designed using the software Solidworks as well, and later tooled using Finite Element Modeling and Post processing software - FEMAP. Using FEMAP, it is possible to test vibration modes, and right after it apply the Modal Cal-culation to study the phases of the mission to ensure structural stiffness and prevent malfunctions and damage to the satellite subsystems. After the calculations, the tests will be applied at the LIT to confront the theo-retical and practical data. This paper also discusses the Process of NANOSATC-BR2 3D Printing for its Mechanical Model, and the influ-ences that the 3D Printer limitations had on the Design of this nanosatellite. The INPE-UFSM's NANOSATC-BR CubeSats Develop-ment Program has been designed and executed in a partnership between the CRS/INPE-MCTI and LACESM/CT-UFSM, to improve Capacity Building in Brazil in Space Science and Technology . The Program has support from the Brazilian Space Agency (AEB).
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4. Conditions of access and use
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Reader Groupadministrator
simone
Visibilityshown
Read Permissionallow from all
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3EUFCFP
8JMKD3MGPCW/446AF4B
Host Collectionsid.inpe.br/mtc-m21b/2013/09.26.14.25.20
6. Notes
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