@InProceedings{SilvaNetoPradSancForm:2016:AlStDi,
               author = "Silva Neto, Jos{\'e} Batista da and Prado, Antonio Fernando 
                         Bertachini de Almeida and Sanchez, Diogo Merguizo and Formiga, J. 
                         K. S.",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)} and {Universidade Estadual Paulista 
                         (UNESP)}",
                title = "Alternative strategy for the disposal of CubeSats in the LEO 
                         region",
            booktitle = "Anais...",
                 year = "2016",
               editor = "Cerqueira, Christopher Shneider and Souza, Alain Giacobini de and 
                         Oliveira Junior, Eloy Martins de and Bertoldo Junior, Jorge and 
                         Yassuda, Irineu dos Santos and Lima, Jeanne Samara dos Santos and 
                         Morais, Marcelo Henrique Essado de and Oliveira, M{\^o}nica 
                         Elizabeth Rocha de and Gondo, Suely Mitsuko Hirakawa and Fornari, 
                         Celso Israel and Toledo, Rafael Cardoso and Fischer, Gustavo 
                         Alexandre Achilles",
         organization = "Workshop em Engenharia e Tecnologias Espaciais, 7. (WETE)",
            publisher = "Instituto Nacional de Pesquisas Espaciais (INPE)",
              address = "S{\~a}o Jos{\'e} dos Campos",
             keywords = "Debris, Discard, CubeSats, Orbital Maneuvers.",
             abstract = "The number of missions involving CubeSats increases each year, 
                         including Brazilian missions. The simplification of the projects 
                         for smaller structures and less weight makes the missions of 
                         CubeSats cheaper compared to large satellites. Also, in recent 
                         years, the concern about the increase of objects in orbit is more 
                         important, since operational satellites and upper stage of 
                         launchers that populate the low orbits region (LEO) are more 
                         numerous. To try to reduce this problem there is a consensus that 
                         objects in LEO region should re-enter in the atmosphere within 25 
                         years. This is becoming a limiting for projects of CubeSats. Thus, 
                         this study presents an alternative to this problem, which is the 
                         use of devices of area augmentation and variation of the 
                         coefficient of reflectivity in a CubeSat. Thus, it is possible, 
                         even in regions where the air density is not sufficiently large or 
                         where there is no more atmosphere, to force the decay of a 
                         CubeSat. Then, one can carry out missions of CubeSat to aim for 
                         higher altitudes than current missions, expanding the 
                         possibilities of applications.",
  conference-location = "S{\~a}o Jos{\'e} dos Campos",
      conference-year = "23-25 ago. 2016",
                 issn = "2177-3114",
             language = "en",
                  ibi = "8JMKD3MGP3W34P/3ME48B5",
                  url = "http://urlib.net/ibi/8JMKD3MGP3W34P/3ME48B5",
           targetfile = "[WETE][2016] Jos{\'e} Batista Silva Neto.pdf",
        urlaccessdate = "12 maio 2024"
}