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On the stability of additional moons orbiting Kepler-1625 b

dc.contributor.authorMoraes, R. A. [UNESP]
dc.contributor.authorBorderes-Motta, G.
dc.contributor.authorWinter, O. C. [UNESP]
dc.contributor.authorMonteiro, J. [UNESP]
dc.contributor.institutionUniversidade Estadual Paulista (UNESP)
dc.contributor.institutionUniversidad Carlos III de Madrid
dc.date.accessioned2022-05-01T15:46:10Z
dc.date.available2022-05-01T15:46:10Z
dc.date.issued2022-02-01
dc.description.abstractSince it was proposed, the exomoon candidate Kepler-1625 b-I has changed the way we see satellite systems. Because of its unusual physical characteristics, many questions about the stability and origin of this candidate have been raised. Currently, we have enough theoretical studies to show that if Kepler-1625 b-I is indeed confirmed, it will be stable. Regarding its origin, previous works indicated that the most likely scenario is capture, although conditions for in situ formation have also been investigated. In this work, we assume that Kepler-1625 b-I is an exomoon and study the possibility of an additional, massive exomoon being stable in the same system. To model this scenario, we perform N-body simulations of a system including the planet, Kepler-1625 b-I, and one extra Earth-like satellite. Based on previous results, the satellites in our system will be exposed to tidal interactions with the planet and to gravitational effects owing to the rotation of the planet. We find that the satellite system around Kepler-1625 b is capable of harbouring two massive satellites. The extra Earth-like satellite can be stable in various locations between the planet and Kepler-1625 b-I, with a preference for regions inside $25\, R_{\rm p}$. Our results suggest that the strong tidal interaction between the planet and the satellites is an important mechanism to ensure the stability of satellites in circular orbits closer to the planet, while the 2:1 mean motion resonance between the Earth-like satellite and Kepler-1625 b-I would provide stability for satellites in wider orbits.en
dc.description.affiliationUNESP Universidade Estadual Paulista Grupo de Dinâmica Orbital and Planetologia, São Paulo
dc.description.affiliationBioengineering and Aerospace Engineering Department Universidad Carlos III de Madrid, LeganCrossed D sign©s
dc.description.affiliationUnespUNESP Universidade Estadual Paulista Grupo de Dinâmica Orbital and Planetologia, São Paulo
dc.format.extent2583-2596
dc.identifierhttp://dx.doi.org/10.1093/mnras/stab3576
dc.identifier.citationMonthly Notices of the Royal Astronomical Society, v. 510, n. 2, p. 2583-2596, 2022.
dc.identifier.doi10.1093/mnras/stab3576
dc.identifier.issn1365-2966
dc.identifier.issn0035-8711
dc.identifier.scopus2-s2.0-85126462985
dc.identifier.urihttp://hdl.handle.net/11449/234272
dc.language.isoeng
dc.relation.ispartofMonthly Notices of the Royal Astronomical Society
dc.sourceScopus
dc.subjectplanets and satellites: dynamical evolution and stability
dc.subjectplanets and satellites: individual: Kepler-1625 b-I
dc.titleOn the stability of additional moons orbiting Kepler-1625 ben
dc.typeArtigopt
dspace.entity.typePublication
relation.isDepartmentOfPublicationcf723ce7-c9ee-4e06-b772-346bd0a102bb
relation.isDepartmentOfPublication.latestForDiscoverycf723ce7-c9ee-4e06-b772-346bd0a102bb
unesp.departmentMatemática - FEGpt

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