@Article{PiñerosPradGome:2018:ReDiPo,
author = "Piñeros, Jhonathan Orlando Murcia and Prado, Antonio Fernando
Bertachini de Almeida and Gomes, Vivian Martins",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)} and {Universidade Estadual
Paulista (UNESP)}",
title = "Retrograde and direct powered aero-gravity-assist trajectories
around mars",
journal = "Revista Mexicana de Astronom{\'{\i}}a y Astrof{\'{\i}}sica",
year = "2018",
volume = "54",
pages = "143--161",
keywords = "Astrodin{\^a}mica, celestial mechanics, planets and satellites:
atmospheres, space vehicles.",
abstract = "A Gravity-Assist maneuver is used to reduce fuel consumption
and/or trip times in interplanetary missions. It is based in a
close approach of a spacecraft to a celestial body. Missions like
Voyager and Ulysses used this concept. The present paper performs
a study of a maneuver that combines three effects: the gravity of
the planet, the application of an impulsive maneuver when the
spacecraft is passing by the periapsis and the effects of the
atmosphere of the planet. Direct and retrograde trajectories are
considered, with particular attention to the differences due to
the higher relative velocity between the spacecraft and the
atmosphere, which increases the effects of the atmosphere. The
planet Mars is used for the numerical examples. RESUMEN: Se emplea
una maniobra asistida por la gravedad para reducir el consumo de
combustible y/o el tiempo de vuelo en misiones interplanetarias.
La maniobra se basa en un acercamiento entre la nave y el planeta.
El Voyager y el Ulysses emplearon este concepto. Aqu´\ı,
estudiamos una maniobra que combina tres efectos: la gravedad del
planeta, la aplicaci´on de un impulso cuando la nave pasa por
periapsis, y los efectos de la atm´osfera del planeta. Se
consideran trayectorias directas y retr´ogradas, con particular
atenci´on en las diferencias causadas por la mayor velocidad
relativa entre la nave y la atm´osfera, las cuales incrementan el
efecto de esta ´ultima. Se presentan ejemplos num´ericos para el
planeta Marte.",
issn = "0185-1101",
label = "lattes: 7340081273816424 2 PiñerosPradGome:2018:REDIPO",
language = "en",
urlaccessdate = "28 abr. 2024"
}