Determination of the force transmitted by an ion thruster plasma plume to an orbital object

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dc.contributor.author Alpatov, A.
dc.contributor.author Cichocki, Filippo
dc.contributor.author Fokov, A.
dc.contributor.author Khoroshylov, S.
dc.contributor.author Merino Martínez, Mario
dc.contributor.author Zakrzhevskii, A.
dc.date.accessioned 2019-11-19T13:28:33Z
dc.date.available 2019-11-19T13:28:33Z
dc.date.issued 2016-02
dc.identifier.bibliographicCitation Acta astronautica, 119, Feb.-March 2016, Pp. 241-251
dc.identifier.issn 0094-5765
dc.identifier.issn 1879-2030 (online)
dc.identifier.uri http://hdl.handle.net/10016/29197
dc.description.abstract An approach to determine the force transmitted by the plasma plume of an ion thruster to an orbital object immersed in it using its central projection on a selected plane is proposed. A photo camera is used to obtain the image of the object central projection. The algorithms for the calculation of the transmission of momentum by the impacting ion beam are developed including the determination of the object contour and the correction of the error due to a camera offset from the ion beam axis, and the computation of the fraction of the ion beam that impinges on the object surface.
dc.description.sponsorship The research leading to these results has received funding from the European Union Seventh Framework Programme (FP7/2007-2013) under grant agreement n°607457.
dc.format.extent 11
dc.language.iso eng
dc.publisher Elsevier Ltd.
dc.rights © 2015 IAA. Published by Elsevier Ltd. All rights reserved.
dc.rights This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.
dc.rights Atribución-NoComercial-SinDerivadas 3.0 España
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.subject.other Electric propulsion
dc.subject.other Plasma plume
dc.subject.other Contactiess
dc.subject.other Space Debris
dc.subject.other Active debris removal
dc.subject.other Ion beam shepherd
dc.subject.other Beam shepherd
dc.title Determination of the force transmitted by an ion thruster plasma plume to an orbital object
dc.type article
dc.subject.eciencia Aeronáutica
dc.subject.eciencia Física
dc.identifier.doi https://doi.org/10.1016/j.actaastro.2015.11.020
dc.rights.accessRights openAccess
dc.relation.projectID info:eu-repo/grantAgreement/EC/FP7/607457/LEOSWEEP
dc.type.version acceptedVersion
dc.identifier.publicationfirstpage 241
dc.identifier.publicationlastpage 251
dc.identifier.publicationtitle ACTA ASTRONAUTICA
dc.identifier.publicationvolume 119
dc.identifier.uxxi AR/0000017698
dc.contributor.funder European Commission
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