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Please use this identifier to cite or link to this item: http://acervodigital.unesp.br/handle/11449/70205
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dc.contributor.authorSolórzano, Carlos Renato Huaura-
dc.contributor.authorDe Almeida Prado, Antonio Fernando Bertachini-
dc.contributor.authorWinter, Othon Cabo-
dc.date.accessioned2014-05-27T11:22:45Z-
dc.date.accessioned2016-10-25T18:25:02Z-
dc.date.available2014-05-27T11:22:45Z-
dc.date.available2016-10-25T18:25:02Z-
dc.date.issued2007-12-01-
dc.identifier.citationAdvances in the Astronautical Sciences, v. 127 PART 1, p. 1043-1060.-
dc.identifier.issn0065-3438-
dc.identifier.urihttp://hdl.handle.net/11449/70205-
dc.identifier.urihttp://acervodigital.unesp.br/handle/11449/70205-
dc.description.abstractThe gravitational capture was initially used to understand the capture of planetary satellites. However, in the 90's decade, this phenomenon was applied in spacecraft trajectories. Belbruno and Miller studied missions in the Earth-Moon system that uses this technique to save fuel during the insertion of the spacecraft in its final orbit around the Moon. Using a parameter defined as twice the two-body energy of the planet-particle system, Yamakawa also studied the gravitational capture in the Earth-Moon system. In the present paper, this technique is used to study a mission that goes to the Neptune system and perform a gravitational capture in the satellite Triton. The results show direct and retrograde trajectories, for different values of the initial conditions.en
dc.format.extent1043-1060-
dc.language.isoeng-
dc.sourceScopus-
dc.subjectInterplanetary flight-
dc.subjectInterplanetary spacecraft-
dc.subjectMoon-
dc.subjectSatellites-
dc.subjectSpacecraft-
dc.subjectTrajectories-
dc.subjectGravitational captures-
dc.subjectInitial conditions-
dc.subjectInterplanetary missions-
dc.subjectNeptune-
dc.subjectParticle systems-
dc.subjectPlanetary satellites-
dc.subjectSpacecraft trajectories-
dc.subjectMechanics-
dc.titleAn interplanetary mission to Neptune system: Gravitational capture and maneuvers around tritonen
dc.typeoutro-
dc.contributor.institutionInstituto Nacional de Pesquisas Espaciais (INPE)-
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)-
dc.description.affiliationInstitute Nacional de Pesquisas Espaciais (INPE), São José dos Campos-SP-12227-010-
dc.description.affiliationUniversidade Estadual Paulista (UNESP-FEG) Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá-SP-12516-4I0-
dc.description.affiliationUnespUniversidade Estadual Paulista (UNESP-FEG) Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá-SP-12516-4I0-
dc.rights.accessRightsAcesso restrito-
dc.relation.ispartofAdvances in the Astronautical Sciences-
dc.identifier.scopus2-s2.0-55549087210-
Appears in Collections:Artigos, TCCs, Teses e Dissertações da Unesp

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