@Article{RibeiroMeirMeloPrad:2023:OpGeLu,
               author = "Ribeiro, Rebeca de Souza and Meireles, Lucas Gouv{\^e}a and Melo, 
                         Cristiano F. de and Prado, Antonio Fernando Bertachini de 
                         Almeida",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Universidade Federal 
                         de Minas Gerais (UFMG)} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)}",
                title = "Optimal geometry for lunar swing-by maneuvers aided by solar sails 
                         in the restricted four-body problem",
              journal = "European Physical Journal-Special Topics",
                 year = "2023",
               volume = "2023",
                pages = "1",
             abstract = "As the geometry of the swing-by maneuver greatly influences the 
                         outcome of the gain of energy and a possible escape trajectory, a 
                         study on the relative positioning between the Earth and the Moon 
                         is presented to define the conditions for the best transfers to 
                         the terrestrial planets of the solar system in the restricted 
                         four-body SunEarthMoonspacecraft Problem. At the start of the 
                         numerical simulation, a solar sail with loading of 164.7 g/m2 is 
                         already deployed to conduct transfers towards Venus and Mars.",
                  doi = "10.1140/epjs/s11734-023-01028-8",
                  url = "http://dx.doi.org/10.1140/epjs/s11734-023-01028-8",
                 issn = "1951-6355",
                label = "lattes: 3242133432342198 2 RibeiroMeirMeloPrad:2023:OpGeLu",
             language = "en",
           targetfile = "s11734-023-01028-8.pdf",
        urlaccessdate = "04 maio 2024"
}