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		<doi>10.1177/0954410011409131</doi>
		<issn>0954-4100</issn>
		<issn>2041-3025</issn>
		<label>lattes: 3979829162351186 3 ColettiGabrMarq:2012:DiHoCa</label>
		<citationkey>ColettiMarqGabr:2012:DiHoCa</citationkey>
		<title>Discharge hollow cathode design for a dual-stage gridded ion engine</title>
		<project>European Community’s Seventh Framework Programme (FP7/2007-2013) under grant agreement number 218859</project>
		<year>2012</year>
		<secondarytype>PRE PI</secondarytype>
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		<size>305 KiB</size>
		<author>Coletti, M.,</author>
		<author>Marques, Rodrigo Intini,</author>
		<author>Gabriel, Stephen B.,</author>
		<group></group>
		<group>LCP-CTE-INPE-MCTI-GOV-BR</group>
		<affiliation>Astronautics Research Group, University of Southampton, Southampton, UK</affiliation>
		<affiliation>Instituto Nacional de Pesquisas Espaciais (INPE)</affiliation>
		<affiliation>Astronautics Research Group, University of Southampton, Southampton, UK</affiliation>
		<electronicmailaddress></electronicmailaddress>
		<electronicmailaddress>intini@lcp.inpe.br</electronicmailaddress>
		<e-mailaddress>intini@lcp.inpe.br</e-mailaddress>
		<journal>Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering</journal>
		<volume>226</volume>
		<number>3</number>
		<pages>272-280</pages>
		<secondarymark>B1_ENGENHARIAS_III</secondarymark>
		<transferableflag>1</transferableflag>
		<contenttype>External Contribution</contenttype>
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		<keywords>hollow cathode, gridded ion engine, GIE, dual stage ion engine, DS4G.</keywords>
		<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.</abstract>
		<area>COMB</area>
		<language>en</language>
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		<notes>Setores de Atividade: Pesquisa e desenvolvimento científico.</notes>
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		<url>http://plutao.sid.inpe.br/rep-/dpi.inpe.br/plutao/2012/11.28.17.33</url>
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