@InProceedings{SouzaPrad:2010:PeCoTh,
author = "Souza, Denilson Paulo Santos de and Prado, A. F. B. A.",
affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto
Nacional de Pesquisas Espaciais (INPE)}",
title = "Performance Comparison between Thrusters PPS1350 and the Phall 1
in Optimal Trajectories using Flybies and Solar Electric
Propulsion",
booktitle = "Proceedings...",
year = "2010",
pages = "435--441",
organization = "WSEAS International Conference on Engineering Mechanics,
Structures, Engineering Geology, 3. (EMESEG '10).",
keywords = "Space Trajectories, Applied Mathematics, Astrodynamics, Celestial
Mechanics, Space Trajectories, Flyby.",
abstract = "The spacecraft propulsion system has passed for diverse
evolutions, leaving combustion engines and arriving at ion
propulsion. The future interplanetary missions will probably use
the conventional chemical rockets to leave the sphere of influence
of the Earth, and solar electric propulsion (SEP) to accomplish
the other maneuvers of the mission. The optimization of maneuvers
will be approached in interplanetary missions using solar electric
propulsion and Gravity Assisted Maneuver attended to reduce the
costs of the mission. Exploring the high specific impulse and the
capacity of the electric propulsion to obtain a Gravity Assisted
Maneuver with the Earth after a year of the departure of the
spacecraft. Shall be analyzed missions with thrusters PPS1350 and
the Phall 1 for performance comparison. An indirect optimization
method will be used in the simulations.",
conference-location = "Corfu Island,",
conference-year = "2010",
isbn = "978-960-474-203-5",
issn = "1792-4294",
language = "en",
targetfile = "Souza_Performance.pdf",
urlaccessdate = "12 maio 2024"
}