@Article{ColettiMarqGabr:2012:DiHoCa,
author = "Coletti, M. and Marques, Rodrigo Intini and Gabriel, Stephen B.",
affiliation = "Astronautics Research Group, University of Southampton,
Southampton, UK and {Instituto Nacional de Pesquisas Espaciais
(INPE)} and Astronautics Research Group, University of
Southampton, Southampton, UK",
title = "Discharge hollow cathode design for a dual-stage gridded ion
engine",
journal = "Proceedings of the Institution of Mechanical Engineers, Part G:
Journal of Aerospace Engineering",
year = "2012",
volume = "226",
number = "3",
pages = "272--280",
note = "{Setores de Atividade: Pesquisa e desenvolvimento
cient{\'{\i}}fico.}",
keywords = "hollow cathode, gridded ion engine, GIE, dual stage ion engine,
DS4G.",
abstract = "At the end of 2008, a European Union-sponsored project called
HiPER (high power electric propulsion: a roadmap for the future)
was started in Europe with the aim of defining the roadmap for the
future of electric propulsion. Within this project, several
different propulsive systems are under study, and among those the
dual-stage gridded ion engine. In this article, starting from the
different thruster configurations highlighted in the HiPER
project, the discharge and neutralizer hollow cathode requirements
will be derived. Subsequently, the design for a discharge hollow
cathode able to satisfy the most current demanding case will be
presented.",
doi = "10.1177/0954410011409131",
url = "http://dx.doi.org/10.1177/0954410011409131",
issn = "0954-4100 and 2041-3025",
label = "lattes: 3979829162351186 3 ColettiGabrMarq:2012:DiHoCa",
language = "en",
urlaccessdate = "30 abr. 2024"
}