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DC Field | Value | Language |
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dc.contributor.author | Solórzano, Carlos Renato Huaura | - |
dc.contributor.author | De Almeida Prado, Antonio Fernando Bertachini | - |
dc.contributor.author | Winter, Othon Cabo | - |
dc.date.accessioned | 2014-05-27T11:22:45Z | - |
dc.date.accessioned | 2016-10-25T18:25:02Z | - |
dc.date.available | 2014-05-27T11:22:45Z | - |
dc.date.available | 2016-10-25T18:25:02Z | - |
dc.date.issued | 2007-12-01 | - |
dc.identifier.citation | Advances in the Astronautical Sciences, v. 127 PART 1, p. 1043-1060. | - |
dc.identifier.issn | 0065-3438 | - |
dc.identifier.uri | http://hdl.handle.net/11449/70205 | - |
dc.identifier.uri | http://acervodigital.unesp.br/handle/11449/70205 | - |
dc.description.abstract | The 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.extent | 1043-1060 | - |
dc.language.iso | eng | - |
dc.source | Scopus | - |
dc.subject | Interplanetary flight | - |
dc.subject | Interplanetary spacecraft | - |
dc.subject | Moon | - |
dc.subject | Satellites | - |
dc.subject | Spacecraft | - |
dc.subject | Trajectories | - |
dc.subject | Gravitational captures | - |
dc.subject | Initial conditions | - |
dc.subject | Interplanetary missions | - |
dc.subject | Neptune | - |
dc.subject | Particle systems | - |
dc.subject | Planetary satellites | - |
dc.subject | Spacecraft trajectories | - |
dc.subject | Mechanics | - |
dc.title | An interplanetary mission to Neptune system: Gravitational capture and maneuvers around triton | en |
dc.type | outro | - |
dc.contributor.institution | Instituto Nacional de Pesquisas Espaciais (INPE) | - |
dc.contributor.institution | Universidade Estadual Paulista (UNESP) | - |
dc.description.affiliation | Institute Nacional de Pesquisas Espaciais (INPE), São José dos Campos-SP-12227-010 | - |
dc.description.affiliation | Universidade Estadual Paulista (UNESP-FEG) Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá-SP-12516-4I0 | - |
dc.description.affiliationUnesp | Universidade Estadual Paulista (UNESP-FEG) Grupo de Dinâmica Orbital e Planetologia, Guaratinguetá-SP-12516-4I0 | - |
dc.rights.accessRights | Acesso restrito | - |
dc.relation.ispartof | Advances in the Astronautical Sciences | - |
dc.identifier.scopus | 2-s2.0-55549087210 | - |
Appears in Collections: | Artigos, TCCs, Teses e Dissertações da Unesp |
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