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  • NANOSATC-BR1 Electrical Power Subsystem – Development of a Power Budget

    Paper number

    IAC-12,C3,4,10,x13765

    Author

    Mr. Dimas Irion Alves, Southern Regional Space Research Center - CRS/CCR/INPE - MCT in collaboration with the Space Science Laboratory of Santa Maria - LACESM/CT - UFSM, Brazil

    Coauthor

    Dr. Nelson Jorge Schuch, Southern Regional Space Research Center - CRS/CCR/INPE - MCT in collaboration with the Space Science Laboratory of Santa Maria - LACESM/CT - UFSM, Brazil

    Coauthor

    Dr. Natanael Rodrigues Gomes, Federal University of Santa Maria, Brazil

    Coauthor

    Dr. Otavio S.C. Durao, The Brazilian Institute for Space Research, Brazil

    Coauthor

    Dr. Renato Machado, Electronic and Computing Department and Santa Maria Space Science Laboratory, ((DELC-LACESM)/CT/UFSM), Brazil, Brazil

    Coauthor

    Mr. Cláudio Machado Paulo, Southern Regional Space Research Center – CRS/CCR/INPE – MCT in collaboration with the Santa Maria Space Science Laboratory – LACESM/CT – UFSM, Brazil, Brazil

    Coauthor

    Mr. Leonardo Zavareze da Costa, Southern Regional Space Research Center - CRS/CCR/INPE - MCT in collaboration with the Space Science Laboratory of Santa Maria - LACESM/CT - UFSM, Brazil

    Year

    2012

    Abstract
    The NANOSATC-BR1 is the first satellite of the Brazilian NANOSATC-BR Program. The NANOSATC-BR1 is a CubeSat with a cubic shape with 10 cm of edges and a mass of approximately 1 kg. The satellite is scheduled for launching in the second half of 2012 in a polar circular orbit. The primary source of electrical power of the satellite is a solar generator compound by solar cells covering the six satellite faces. Due to the very low power capability of the solar generator, an accurate study of the generated and consumed energy is necessary to assure balanced and safe satellite operation. To obtain accurate prevision of the illuminated and eclipse periods, simulations were performed. In order to obtain accurate analysis of generated and consumed power, a model of the satellite was developed, and simulations were performed using electronic simulation software. This work presents the NANOSATC-BR1’ electrical power subsystem, and results of the electrical power model simulation, considering begin-of-life (BOL) conditions of the satellite for different load conditions and operation periods.
    Abstract document

    IAC-12,C3,4,10,x13765.brief.pdf

    Manuscript document

    IAC-12,C3,4,10,x13765.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.