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dc.contributor.authorDutta, Atri
dc.contributor.authorKasdin, N. Jeremy
dc.contributor.authorChoueiri, Edgar Y.
dc.contributor.authorFrancken, Philippe
dc.date.accessioned2016-05-31T15:36:10Z
dc.date.available2016-05-31T15:36:10Z
dc.date.issued2016-04
dc.identifier.citationAtri Dutta, N. Jeremy Kasdin, Edgar Choueiri, and Philippe Francken. "Minimizing Proton Displacement Damage Dose During Electric Orbit Raising of Satellites", Journal of Guidance, Control, and Dynamics, Vol. 39, No. 4 (2016), pp. 963-969en_US
dc.identifier.issn0731-5090
dc.identifier.otherWOS:000374861000020
dc.identifier.urihttp://dx.doi.org/10.2514/1.G000503
dc.identifier.urihttp://hdl.handle.net/10057/12053
dc.descriptionClick on the DOI link to access the Article (may not be free).en_US
dc.description.abstractAlthough electric propulsion systems have been used in deep space missions for performing interplanetary transfers, their use has primarily been restricted to station-keeping purposes for Earth-orbiting satellites. Geosynchronous equatorial orbit (GEO) satellites have mostly used chemical thrusters to transfer to GEO from an initial orbit into which it is launched by an appropriate launch vehicle.en_US
dc.description.sponsorshipThis work was performed under grant number AGMT dated 1 April 2011 from SES Engineering.en_US
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.ispartofseriesJournal of Guidance, Control, and Dynamics;v.39:no.4
dc.subjectPropulsionen_US
dc.titleMinimizing proton displacement damage dose during electric orbit raising of satellitesen_US
dc.typeArticleen_US
dc.rights.holderCopyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US


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  • AE Research Publications [114]
    Research publications authored by the Department of Aerospace Engineering faculty and graduate students.

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