2026-09-19T08:50:01Zhttps://dspace.mit.edu/server/oai/requestoai:dspace.mit.edu:1721.1/906682022-01-13T07:53:53Zcom_1721.1_7582com_1721.1_7581col_1721.1_131023
Alvar Saenz-Otero.
Hayhurst, Dustin Luke
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
2014-10-08T15:21:34Z
2014-10-08T15:21:34Z
2014
http://hdl.handle.net/1721.1/90668
890461168
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2014.
Cataloged from PDF version of thesis. "June 2014." "This material is declared a work of the United States Government and is not subject to copyright protection in the United States."
Includes bibliographical references (pages 101-102).
Understanding fluid slosh in a microgravity environment has the potential to make liquid-fueled spacecraft more effective. The SPHERES-Slosh Experiment gathers benchmarking data that can be used to validate computational fluid dynamics models for microgravity environments. This thesis discusses the design of the SSE hardware and the control theory used on the International Space Station during test sessions. This thesis proposes future control theory and design work.
by Dustin Luke Hayhurst.
S.M.
102 pages
eng
Massachusetts Institute of Technology
M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
http://dspace.mit.edu/handle/1721.1/7582
Aeronautics and Astronautics.
Development and Implementation of the SPHERES-Slosh Experiment
Thesis
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