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dc.contributor.advisorPaulo Lozano.en_US
dc.contributor.authorApodaca Moreno, Maria Regina.en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2021-01-06T18:33:17Z
dc.date.available2021-01-06T18:33:17Z
dc.date.copyright2020en_US
dc.date.issued2020en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/129185
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, September, 2020en_US
dc.descriptionCataloged from student-submitted PDF of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 75-76).en_US
dc.description.abstractIonic liquids (ILs) are molten salts that are used in electrospray thrusters as the source for the ionic emission. The total current of the emitted ions is proportional to the conductivity and the surface tension of the ionic liquid. Since the thrust of the propulsion system is dependent on the current, we try to maximize the total current emitted. However, the production of new ionic liquids is very challenging and thus this thesis explores the use of mixtures as an alternative ionic source. This thesis studies the relationship that exists between temperature, conductivity and surface tension with the concentration of LiBF₄ salt in the EMIBF₄ ionic liquid. The solvent was selected given it is one of the most commonly used ionic liquids in electrospray propulsion. The salt, on the other hand, was selected because of its small and simple positive ion Li⁺ and its matching negative ion, BF⁻₄ to that of the IL. From measurements at a concentration of 27wt% time of flight spectrometer, an increase in the percentage of the beam that was single EMI⁺ from ~ 50% to ~ 70%. This lead to an increase in efficiency of ~ 2% and specific impulse of ~ 27%. It was found that the surface tension of the mixture decreases as the concentration increases. Likewise, the conductivity tends to decrease as the weight percentage of salt is increased, except for a local maximum around 15wt%.en_US
dc.description.statementofresponsibilityby Maria Regina Apodaca Moreno.en_US
dc.format.extent76 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleIonic liquid and lithium salt mixtures as ionic sourcesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc1227278419en_US
dc.description.collectionS.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2021-01-06T18:33:15Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentAeroen_US


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