Gravitational Capture of Asteroids by Gas Drag


Autoria(s): Vieira Neto, E.; Winter, O. C.
Contribuinte(s)

Universidade Estadual Paulista (UNESP)

Data(s)

20/05/2014

20/05/2014

01/01/2009

Resumo

Fundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

Several irregular satellites of the giant planets were found in the last years. Their orbital configuration suggests that these satellites were asteroids captured by the planets. The restricted three-body problem can explain the dynamics of the capture, but the capture is temporary. It is necessary some kind of dissipative effect to turn the temporary capture into a permanent one. In this work we study an asteroid suffering a gas drag at an extended atmosphere of a planet to turn a temporary capture into a permanent one. In the primordial Solar System, gas envelopes were created around the planet. An asteroid that was gravitationally captured by the planet got its velocity reduced and could been trapped as an irregular satellite. It is well known that, depending on the time scale of the gas envelope, an asteroid will spiral and collide with the planet. So, we simulate the passage of the asteroid in the gas envelope with its density decreasing along the time. Using this approach, we found effective captures, and have a better understanding of the whole process. Finally, we conclude that the origin of the irregular satellites cannot be attributed to the gas drag capture mechanism alone. Copyright (C) 2009 E. Vieira Neto and O.C. Winter.

Formato

11

Identificador

http://dx.doi.org/10.1155/2009/897570

Mathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 11, 2009.

1024-123X

http://hdl.handle.net/11449/9300

10.1155/2009/897570

WOS:000276147100001

WOS000276147100001.pdf

Idioma(s)

eng

Publicador

Hindawi Publishing Corporation

Relação

Mathematical Problems in Engineering

Direitos

openAccess

Tipo

info:eu-repo/semantics/article