Dynamics of Space Particles and Spacecrafts Passing by the Atmosphere of the Earth

dc.contributorUniversidade Estadual Paulista (Unesp)
dc.contributorInstituto Nacional de Pesquisas Espaciais (INPE)
dc.contributorAdam Mickiewicz Univ
dc.creatorGomes, Vivian Martins [UNESP]
dc.creatorBertachini de Almeida Prado, Antonio Fernando
dc.creatorGolebiewska, Justyna
dc.date2014-12-03T13:09:14Z
dc.date2014-12-03T13:09:14Z
dc.date2013-01-01
dc.date.accessioned2023-09-09T09:54:02Z
dc.date.available2023-09-09T09:54:02Z
dc.identifierhttp://dx.doi.org/10.1155/2013/489645
dc.identifierScientific World Journal. New York: Hindawi Publishing Corporation, 6 p., 2013.
dc.identifier1537-744X
dc.identifierhttp://hdl.handle.net/11449/112105
dc.identifier10.1155/2013/489645
dc.identifierWOS:000328772200001
dc.identifierWOS000328772200001.pdf
dc.identifier6880903376164690
dc.identifier.urihttps://repositorioslatinoamericanos.uchile.cl/handle/2250/8761742
dc.descriptionThe present research studies the motion of a particle or a spacecraft that comes from an orbit around the Sun, which can be elliptic or hyperbolic, and that makes a passage close enough to the Earth such that it crosses its atmosphere. The idea is to measure the Sun-particle two-body energy before and after this passage in order to verify its variation as a function of the periapsis distance, angle of approach, and velocity at the periapsis of the particle. The full system is formed by the Sun, the Earth, and the particle or the spacecraft. The Sun and the Earth are in circular orbits around their center of mass and the motion is planar for all the bodies involved. The equations of motion consider the restricted circular planar three-body problem with the addition of the atmospheric drag. The initial conditions of the particle or spacecraft (position and velocity) are given at the periapsis of its trajectory around the Earth.
dc.descriptionConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)
dc.descriptionFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.descriptionCoordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)
dc.descriptionUniv Estadual Paulista, FEG UNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.descriptionInst Nacl Pesquisas Espaciais, BR-12227010 Sao Jose Dos Campos, SP, Brazil
dc.descriptionAdam Mickiewicz Univ, Fac Phys, Astron Observ Inst, PL-60286 Poznan, Poland
dc.descriptionUniv Estadual Paulista, FEG UNESP, Grp Dinam Orbital & Planetol, BR-12516410 Guaratingueta, SP, Brazil
dc.descriptionCNPq: 473387/2012-3
dc.descriptionCNPq: 304700/2009-6
dc.descriptionFAPESP: 11/09310-7
dc.descriptionFAPESP: 11/08171-3
dc.descriptionFAPESP: 11/13101-4
dc.format6
dc.languageeng
dc.publisherHindawi Publishing Corporation
dc.relationScientific World Journal
dc.rightsAcesso aberto
dc.sourceWeb of Science
dc.titleDynamics of Space Particles and Spacecrafts Passing by the Atmosphere of the Earth
dc.typeArtigo


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