@Article{MantovaniMMBSDMS:2018:NA2Un,
author = "Mantovani, Lorenzzo Q. and Marques, Rodrigo P. and M{\"u}ller, A.
and Barreto, Eduardo X. and Silva, Andr{\'e} L. and Dur{\~a}o,
Ot{\'a}vio Santos Cupertino and Mattiello-Francisco, Maria de
F{\'a}tima and Schuch, Nelson Jorge",
affiliation = "{Universidade Federal de Santa Maria (UFSM)} and {Universidade
Federal de Santa Maria (UFSM)} and {Universidade Federal de Santa
Maria (UFSM)} and {Universidade Federal de Santa Maria (UFSM)} and
{Universidade Federal de Santa Maria (UFSM)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)} and {Instituto Nacional de Pesquisas
Espaciais (INPE)}",
title = "NANOSATC-BR2, 2 unit CubeSat, power analysis, solar flux
prediction, design and 3D printing of the flight model from the
UFSM \& INPE’S NANOSATC-BR, CubeSat development program",
journal = "Advances in the Astronautical Sciences",
year = "2018",
volume = "163",
pages = "101--112",
note = "4th IAA Conference on University Satellite Missions and CubeSat
Workshop, 2017; Roma; Italy; 4 December 2017",
abstract = "In order to space missions work properly, it is necessary to
previously simulate its behavior in space. The main purpose of
this work is to predict the orbit behavior of a 2 Unit CubeSat by
simulating its flight using a MATLAB code. With this starting
point, it is possible to perform a Power Analysis for the
satellite and analyze the incident thermal radiation on it for a
future Thermal Analysis. In order to help students better
understand the CubeSat model and its components, the flight model
was designed and 3D printed. The NANOSATC-BR2 is the second
nanosatellite from the program NANOSATC-BR, Development of
CubeSats Program.",
issn = "0065-3438.",
language = "en",
urlaccessdate = "03 jun. 2024"
}