Development and Implementation of the SPHERES-Slosh Experiment

Author(s)
Hayhurst, Dustin Luke
Thumbnail
DownloadFull printable version (7.802Mb)
Other Contributors
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Advisor
Alvar Saenz-Otero.
Terms of use
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
Metadata
Show full item record
Abstract
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.
Description
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).
 
Date issued
2014
URI
http://hdl.handle.net/1721.1/90668
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics.
Collections