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dc.contributor.authorDeSouza, Nelsoneng
dc.contributor.authorBenwell, Andrew L., 1980-eng
dc.contributor.authorKovaleski, Scott D.eng
dc.contributor.corporatenameUniversity of Missouri-Columbia. Office of Undergraduate Researcheng
dc.contributor.meetingnameUndergraduate Research and Creative Achievements Forum (2008 : University of Missouri--Columbia)eng
dc.date2008eng
dc.date.issued2008eng
dc.descriptionAbstract only availableeng
dc.description.abstractFerroelectric thrusters can be used in applications where small thrusts are useful such as guiding the movement of satellites. The Pulsed Power and Plasma Science group in the Electrical and Computer Engineering department at MU is characterizing a ferroelectric thruster in order to determine its range of maximum thrust. The thrust is measured using a Michelson interferometer and is in the order of 100µN. Both applied frequency and voltage directly affect the amount of thrust generated, and these variables will be varied to create a thrust operation curve. The thrust measurement technique and the resulting thrust curve is presented.eng
dc.description.sponsorshipCollege of Engineering Undergraduate Research Optioneng
dc.identifier.urihttp://hdl.handle.net/10355/1883eng
dc.languageen_USeng
dc.publisherUniversity of Missouri--Columbia. Office of Undergraduate Researcheng
dc.relation.ispartof2008 Undergraduate Research and Creative Achievements Forum (MU)eng
dc.relation.ispartofcommunityUniversity of Missouri-Columbia. Office of Undergraduate Research. Undergraduate Research and Creative Achievements Forumeng
dc.subjectsatellite propulsioneng
dc.subjectmaximum thrusteng
dc.subjectthrust operation curveeng
dc.titleThrust measurements of a ferroelectric plasma source [abstract]eng
dc.typePresentationeng


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