@Article{SantanaMeloMacaWint:2016:ExMoGr,
author = "Santana, Saymon Henrique Santos and Melo, Cristiano Fiorilo de and
Macau, Elbert Einstein Nehrer and Winter, Othon Cabo",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and
{Universidade Federal do ABC (UFABC)} and {Instituto Nacional de
Pesquisas Espaciais (INPE)} and {Universidade Estadual Paulista
(UNESP)}",
title = "Exploring the Moon gravity to escape from the Earth-Moon system",
journal = "Computational and Applied Mathematics",
year = "2016",
volume = "35",
number = "3",
pages = "701--710",
month = "Oct.",
keywords = "Swing-by, Escape trajectories, Numerical simulations.",
abstract = "Escape trajectories from the Earth-Moon system can be obtained
through a single gravity assist maneuver of a spacecraft with the
Moon. This paper presents a semi-analytical study of variations in
the semi-major axis and the eccentricity of a spacecraft for a
geocentric frame-before and after a close encounter of the
spacecraft with the Moon. Studies on the swing-by dynamics between
a spacecraft and the Moon were performed in order to establish a
set of initial conditions in terms of eccentricities and
semi-major axes of geocentric initial orbits. This way, it was
possible identify which orbits, launched from Earth parking
orbits, accomplish swing-bys with the Moon and generate escape
trajectories.",
doi = "10.1007/s40314-015-0287-3",
url = "http://dx.doi.org/10.1007/s40314-015-0287-3",
issn = "2238-3603",
language = "en",
targetfile = "santana_exploring.pdf",
urlaccessdate = "28 abr. 2024"
}