Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263

Detalhes bibliográficos
Autor(a) principal: Silva Neto, J. B.
Data de Publicação: 2016
Outros Autores: Sanchez, D. M., Prado, A. F.B.A., Formiga, J. K.S. [UNESP]
Tipo de documento: Artigo de conferência
Idioma: eng
Título da fonte: Repositório Institucional da UNESP
Texto Completo: http://hdl.handle.net/11449/169283
Resumo: The number of missions which with an asteroid as a target has increased and this type of exploration will become even more frequent in the future. Space missions require high costs and methods that may reduce them should be studied. An alternative is the use of solar radiation pressure, using a solar sail or similar devices. This study presents a solution for the final phase of the Aster mission, which aims to collide a probe with the surface of the body Alpha of the system 2001SN263 using solar radiation pressure. As noted during the study, the low gravity of the system makes it very sensitive to solar radiation pressure. The high angular velocity of Gamma around Alpha causes collisions and involuntary gravity assisted maneuvers, which are obstacles in the search of initial conditions for the use of such devices.
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spelling Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263The number of missions which with an asteroid as a target has increased and this type of exploration will become even more frequent in the future. Space missions require high costs and methods that may reduce them should be studied. An alternative is the use of solar radiation pressure, using a solar sail or similar devices. This study presents a solution for the final phase of the Aster mission, which aims to collide a probe with the surface of the body Alpha of the system 2001SN263 using solar radiation pressure. As noted during the study, the low gravity of the system makes it very sensitive to solar radiation pressure. The high angular velocity of Gamma around Alpha causes collisions and involuntary gravity assisted maneuvers, which are obstacles in the search of initial conditions for the use of such devices.Board of the Graduate School National Institute for Space Research - INPE, Av. Astronautas, 1758Institute of Science and Technology São Paulo State University (UNESP/ICT)Institute of Science and Technology São Paulo State University (UNESP/ICT)National Institute for Space Research - INPEUniversidade Estadual Paulista (Unesp)Silva Neto, J. B.Sanchez, D. M.Prado, A. F.B.A.Formiga, J. K.S. [UNESP]2018-12-11T16:45:12Z2018-12-11T16:45:12Z2016-01-01info:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/conferenceObject3789-3804Advances in the Astronautical Sciences, v. 158, p. 3789-3804.0065-3438http://hdl.handle.net/11449/1692832-s2.0-85007303837Scopusreponame:Repositório Institucional da UNESPinstname:Universidade Estadual Paulista (UNESP)instacron:UNESPengAdvances in the Astronautical Sciences0,187info:eu-repo/semantics/openAccess2021-10-23T21:44:26Zoai:repositorio.unesp.br:11449/169283Repositório InstitucionalPUBhttp://repositorio.unesp.br/oai/requestopendoar:29462021-10-23T21:44:26Repositório Institucional da UNESP - Universidade Estadual Paulista (UNESP)false
dc.title.none.fl_str_mv Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
title Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
spellingShingle Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
Silva Neto, J. B.
title_short Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
title_full Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
title_fullStr Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
title_full_unstemmed Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
title_sort Using solar radiation pressure to maneuver a spacecraft in the triple asteroid 2001SN263
author Silva Neto, J. B.
author_facet Silva Neto, J. B.
Sanchez, D. M.
Prado, A. F.B.A.
Formiga, J. K.S. [UNESP]
author_role author
author2 Sanchez, D. M.
Prado, A. F.B.A.
Formiga, J. K.S. [UNESP]
author2_role author
author
author
dc.contributor.none.fl_str_mv National Institute for Space Research - INPE
Universidade Estadual Paulista (Unesp)
dc.contributor.author.fl_str_mv Silva Neto, J. B.
Sanchez, D. M.
Prado, A. F.B.A.
Formiga, J. K.S. [UNESP]
description The number of missions which with an asteroid as a target has increased and this type of exploration will become even more frequent in the future. Space missions require high costs and methods that may reduce them should be studied. An alternative is the use of solar radiation pressure, using a solar sail or similar devices. This study presents a solution for the final phase of the Aster mission, which aims to collide a probe with the surface of the body Alpha of the system 2001SN263 using solar radiation pressure. As noted during the study, the low gravity of the system makes it very sensitive to solar radiation pressure. The high angular velocity of Gamma around Alpha causes collisions and involuntary gravity assisted maneuvers, which are obstacles in the search of initial conditions for the use of such devices.
publishDate 2016
dc.date.none.fl_str_mv 2016-01-01
2018-12-11T16:45:12Z
2018-12-11T16:45:12Z
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dc.identifier.uri.fl_str_mv Advances in the Astronautical Sciences, v. 158, p. 3789-3804.
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identifier_str_mv Advances in the Astronautical Sciences, v. 158, p. 3789-3804.
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