@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 abr. 2024"
}