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Gravity assisted Orbital Maneuvers for missions to asteroids

Grant number: 16/18613-7
Support type:Scholarships in Brazil - Master
Effective date (Start): March 01, 2017
Effective date (End): February 28, 2018
Field of knowledge:Engineering - Aerospace Engineering - Flight Dynamics
Cooperation agreement: Coordination of Improvement of Higher Education Personnel (CAPES)
Principal researcher:Antônio Fernando Bertachini de Almeida Prado
Grantee:Rodolfo Batista Negri
Home Institution: Instituto Nacional de Pesquisas Espaciais (INPE). Ministério da Ciência, Tecnologia, Inovações e Comunicações (Brasil). São José dos Campos , SP, Brazil
Associated research grant:11/08171-3 - Orbital dynamics of minor bodies, AP.TEM

Abstract

It is believed that most asteroids retain information about the composition of the Solar System. In this sense, it is very important to study these bodies.Asteroids are also sources of rare minerals and chemicals. Despite this interest, few space missions to asteroids have been launched to date.Thus, the Aster mission arises, consisting in sending a space vehicle to an asteroid. This is a large project involving several Brazilian institutions such as INPE, UNESP, UNB, ON, UFABC, UFRJ, USP, UFPr, UEFS, ITA, IMT, Unicamp, UFF and MAST. In addition to scientific knowledge, many technology products are expected from this mission, such as the validation of various equipment, drivers, etc., as well as the training of human resources. The mission is now under feasibility studies. One of the most important steps for this phase of the mission, the current phase of the project, It is to study the most economical way of sending the spacecraft to the desired asteroid. One of the considered forms to do that is to use a close passage by the Moon. Thus, this paper will consider this type of operation with the use of two models. Assuming the system as modeled by the restricted three body problem and by using the "Patched Conics", dividing the problem into three problems of two bodies (vehicle-Earth, Moon and vehicle-vehicle-Earth). There are no comparative studies of these models for the three-dimensional case. (AU)

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Scientific publications
(References retrieved automatically from Web of Science and SciELO through information on FAPESP grants and their corresponding numbers as mentioned in the publications by the authors)
NEGRI, RODOLFO BATISTA; SUKHANOV, ALEXANDER; BERTACHINI DE ALMEIDA PRADO, ANTONIO FERNANDO. Lunar gravity assists using patched-conics approximation, three and four body problems. Advances in Space Research, v. 64, n. 1, p. 42-63, JUL 1 2019. Web of Science Citations: 1.

Please report errors in scientific publications list by writing to: cdi@fapesp.br.