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@InProceedings{MarquesDSMSFPCMMMDCMS:2016:MoAn3D,
               author = "Marques, Rodrigo Passos and Dutra, Viktor Bizarro and Slongo, 
                         Artur Gustavo and Mantovani, Lorenzo Quevedo and Santos, Thaffarel 
                         and Farias, Tiago and Piovesan, T{\'a}lis and Costa, Leonardo 
                         Zavareze da and Moro, Pietro Fernando and M{\^a}nica, Thales 
                         Ramos and M{\"u}ller, Alex and Dur{\~a}o, Ot{\'a}vio Santos 
                         Cupertino and Caetano, Nattan Roberto and Machado, Renato and 
                         Schuch, Nelson Jorge",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {} and 
                         {Instituto Nacional de Pesquisas Espaciais (INPE)} and {} and {} 
                         and {} and {} and {Instituto Nacional de Pesquisas Espaciais 
                         (INPE)} and {} and {} and {} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)} and {} and {} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "Study of rigid structure vibrations and mechanical modeling for 
                         the NANOSATC-BR2: modal analysis and 3D printing considerations",
                 year = "2016",
         organization = "Latin American IAA CubeSat Workshop, 2.",
             abstract = "The 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).",
  conference-location = "Florian{\'o}polis, SC",
      conference-year = "28 Feb. - 02 Mar.",
        urlaccessdate = "27 nov. 2020"
}


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