Modelling of a radio frequency plasma bridge neutralizer (RFPBN)
dc.bibliographicCitation.firstPage | 9 | |
dc.bibliographicCitation.journalTitle | Procedia engineering | eng |
dc.bibliographicCitation.lastPage | 16 | |
dc.bibliographicCitation.volume | 185 | |
dc.contributor.author | Scholze, F. | |
dc.contributor.author | Eichhorn, C. | |
dc.contributor.author | Bundesmann, C. | |
dc.contributor.author | Spemann, D. | |
dc.contributor.author | Neumann, H. | |
dc.contributor.author | Bulit, A. | |
dc.contributor.author | Feili, D. | |
dc.contributor.author | Gonzalez del Amo, J. | |
dc.date.accessioned | 2023-01-20T08:11:29Z | |
dc.date.available | 2023-01-20T08:11:29Z | |
dc.date.issued | 2017 | |
dc.description.abstract | A performance model of a radio frequency plasma bridge neutralizer was developed to calculate the electrical parameters and optimize the neutralizer design. Minimization of power losses and gas consumption, and a maximization of the neutralizer lifetime and the reliability of the system are requirements of all electric propulsion concepts and strongly determine their future application. The requirements of the neutralizer depend on mission profiles. | eng |
dc.description.version | publishedVersion | eng |
dc.identifier.uri | https://oa.tib.eu/renate/handle/123456789/10961 | |
dc.identifier.uri | http://dx.doi.org/10.34657/9987 | |
dc.language.iso | eng | |
dc.publisher | Amsterdam [u.a.] : Elsevier | |
dc.relation.doi | https://doi.org/10.1016/j.proeng.2017.03.284 | |
dc.relation.essn | 1877-7058 | |
dc.rights.license | CC BY-NC-ND 4.0 Unported | |
dc.rights.uri | https://creativecommons.org/licenses/by-nc-nd/4.0/ | |
dc.subject.ddc | 670 | |
dc.subject.gnd | Konferenzschrift | ger |
dc.subject.other | control laws: Earth-Moon system | eng |
dc.subject.other | libration point | eng |
dc.subject.other | low thrust propulsion | eng |
dc.subject.other | shaded areas | eng |
dc.subject.other | spacecraft | eng |
dc.title | Modelling of a radio frequency plasma bridge neutralizer (RFPBN) | eng |
dc.type | Article | eng |
dc.type | Text | eng |
dcterms.event | 6th Russian-German Conference on Electric Propulsion and Their Application, AUG 28-SEP 02, 2016, Samara, RUSSIA | |
tib.accessRights | openAccess | eng |
wgl.contributor | IOM | |
wgl.subject | Ingenieurwissenschaften | ger |
wgl.subject | Physik | ger |
wgl.type | Zeitschriftenartikel | ger |
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