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dc.contributor.authorDutta, Atri
dc.contributor.authorKasdin, N. Jeremy
dc.contributor.authorChoueiri, Edgar Y.
dc.contributor.authorFrancken, Philippe
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.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.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.ispartofseriesJournal of Guidance, Control, and Dynamics;v.39:no.4
dc.titleMinimizing proton displacement damage dose during electric orbit raising of satellitesen_US
dc.rights.holderCopyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.en_US

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