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Journal of Astrophysics & Aerospace Technology | ISSN: 2329-6542 | Volume 6
Planetary Science and Particle Physics
International Conference on
August 27-28, 2018 | Boston, USA
Mean motion resonances and gravitational captures within the context of planetary migration – the solar
system small bodies’ allocation mechanisms
Helton da Silva Gaspar
Universidade Federal de Santa Catarina, Brazil
T
he solar system current configuration is different than that of the final stage of planets formation. Many solar system features
evinces that the planets past a period of migration which resulted the current orbits. Planetary migration is mainly due the angular
momentum exchange. When two astronomical bodies undergo a close encounter, one of them experiences an orbital rising whilst
the other suffers an orbital shrinkage. Close encounters between a planet and a planetesimal causes the planet a negligible variation
of angular momentum in comparison to the small body. However, when a planet undergoes some billions of such encounters, the net
result is remarkable. Lunar craters, for instance, are evidences of a late heavy bombardment (LHB) by small bodies thrown toward
the terrestrial region during the planetary migration phase. Another strong evidence, are the existence of dozens of irregular satellites
around the giant planets. They are satellites that did not form around their planets. Instead, they were gravitationally captured.
Spectral analysis shows that the composition of many irregular satellites are similar both to the compositions of asteroids found
within the main belt and the Kuiper belt. In special, there are two groups of small bodies with similar spectra: the resonant group
of asteroids Hilda in the asteroid belt, and the Himalias, a dynamical family of Jovian irregular satellites. This work intends to assess
whether the mean motion resonances are capable of connecting the origins of Hilda's and Himalia's and other small bodies that once
orbited the region beyond Jupiter's orbit.
helton.s.gaspar@ufsc.brJ Astrophys Aerospace Technol 2018, Volume 6
DOI: 10.4172/2329-6542-C2-021