Skip navigation
Use este identificador para citar ou linkar para este item: http://repositorio.unb.br/handle/10482/24801
Arquivos associados a este item:
Arquivo Descrição TamanhoFormato 
ARTIGO_PermanentMagnetHall.pdf1,41 MBAdobe PDFVisualizar/Abrir
Registro completo de metadados
Campo DCValorIdioma
dc.contributor.authorMoraes, Brunno Silva-
dc.contributor.authorFerreira, José Leonardo-
dc.contributor.authorFerreira, Ivan Soares-
dc.contributor.authorWinter, Othon Cabo-
dc.contributor.authorMourão, Décio Cardozo-
dc.date.accessioned2017-10-11T14:28:47Z-
dc.date.available2017-10-11T14:28:47Z-
dc.date.issued2014-
dc.identifier.citationMORAES, Brunno Silva et al. A permanent magnet hall thruster for pulsed orbit control of lunar polar satellites. Journal of Physics: Conference Series, v. 511, Article 012074, p. 012074-012074, 2014. Disponível em: <http://iopscience.iop.org/article/10.1088/1742-6596/511/1/012074/meta;jsessionid=FC9C80287FAAA341128A725D7CAE5E5D.c4.iopscience.cld.iop.org>. Acesso em: 11 out. 2017. doi: 10.1088/1742-6596/511/1/012074.pt_BR
dc.identifier.urihttp://repositorio.unb.br/handle/10482/24801-
dc.language.isoInglêspt_BR
dc.publisherIOPsciencept_BR
dc.rightsAcesso Abertopt_BR
dc.titleA permanent magnet hall thruster for pulsed orbit control of lunar polar satellitespt_BR
dc.typeArtigopt_BR
dc.subject.keywordSatélitespt_BR
dc.subject.keywordGravidade (Física) - mediçãopt_BR
dc.rights.licenseContent from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI. Fonte: http://iopscience.iop.org/article/10.1088/1742-6596/511/1/012074/meta;jsessionid=FC9C80287FAAA341128A725D7CAE5E5D.c4.iopscience.cld.iop.org. Acesso em: 11 out. 2017.pt_BR
dc.identifier.doihttps://dx.doi.org/10.1088/1742-6596/511/1/012074pt_BR
dc.description.abstract1Future Moon missions devoted to Lunar surface remote sensing, for example, will require very _ne and accurate orbit control. It is well known that Lunar satellites in polar orbits will su_er a high increase on the eccentricity due to the gravitational perturbation of the Earth. Without proper orbit correction the satellite lifetime will decrease and end up in a collision with the Moon surface. It is pointed out by many authors that this e_ect is a natural consequence of the Lidov-Kozai resonance. We studied di_erent arcs of active lunar satellite propulsion, centered on the orbit apoapsis or periapsis, in order to be able to introduce a correction of the eccentricity at each cycle. The proposed method is based on an approach intended to keep the orbital eccentricity of the satellite at low values.pt_BR
Aparece nas coleções:Artigos publicados em periódicos e afins

Mostrar registro simples do item Visualizar estatísticas



Os itens no repositório estão protegidos por copyright, com todos os direitos reservados, salvo quando é indicado o contrário.