@Article{MeloMacaWintViei:2007:NuStAb,
author = "Melo, Cristiano Fiorilo and Macau, Elbert Einstein Nehrer and
Winter, O. C. and Vieira Neto, E.",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Grupo de
Din{\^a}mica Orbital e Planetologia (UNESP)} and {Grupo de
Din{\^a}mica Orbital e Planetologia (UNESP)}",
title = "Numerical study about natural escape and capture routes by the
moon via lagrangian points L1 and L2",
journal = "Advances in Space Research",
year = "2007",
volume = "In press",
keywords = "Astrodynamics, Earth-Moon Transfer, Mission Design, Orbital
Maneuvers.",
abstract = "The lunar sphere of influence, whose radius is some 66300km, has
regions of stable orbits around the Moon and also regions that
contain trajectories which, after spending some time around the
Moon, escape and are later recaptured by lunar gravity. Both the
escape and the capture occur along the Lagrangian equilibrium
points L1 and L2. In this study, we mapped out the region of lunar
influence considering the restricted three-body Earth-Moonparticle
problem and the four-body Sun-Earth-Moon-particle (probe) problem.
We identified the stable trajectories, and the escape and capture
trajectories through the L1 and L2 in plots of the eccentricity
versus the semi-major axis as a function of the time that the
energy of the osculating lunar trajectory in the two-body
Moon-particle problem remains negative. We also investigated the
properties of these routes, giving special attention to the fact
that they supply a natural mechanism for performing low-energy
transfers between the Earth and the Moon, and can thus be useful
on a great number of future missions.",
issn = "0273-1177",
language = "en",
targetfile = "numerical study.pdf",
urlaccessdate = "01 maio 2024"
}