{"id":{"repo_id":"nps","oai_identifier":"oai:calhoun.nps.edu:10945/37548"},"canonical_url":"https://search.dev.ndltd.org/etd/nps/oai:calhoun.nps.edu:10945/37548","repository":{"repo_id":"nps","name":"Naval Postgraduate School","base_url":"https://calhoun.nps.edu/server/oai/request"},"display":{"title":"The effects of liquid propellant motion on the attitude stability of spin stabilized space-craft","abstract":"An analysis of the effects of liquid motion on the attitude stability of spin stabilized spacecraft is presented. The effects of varying the fuel load and the asymmetry of the platform are emphasized. The energy sink stability criteria are compared to the results of a computer simulation. Based on this comparison the limitations of the energy sink stability criteria are identified.","abstract_html":"An analysis of the effects of liquid motion on the attitude stability of spin stabilized spacecraft is presented. The effects of varying the fuel load and the asymmetry of the platform are emphasized. The energy sink stability criteria are compared to the results of a computer simulation. Based on this comparison the limitations of the energy sink stability criteria are identified.","abstract_has_math":false,"creators":["Myers, Jack W. Jr."],"institution":"Monterey, California. Naval Postgraduate School","degree_name":null,"degree_level":null,"degree_discipline":null,"degree_department":"Department of Aeronautics and Astronautics","school":null,"contributors":[],"advisors":["Agrawal, Brij N."],"committee_chairs":[],"committee_members":[],"year":1990,"date_issued":"1990-03","date_published":"1990-03","updated_at":"2026-07-27T20:26:38Z","subjects":[],"languages":["en_US"],"rights":["This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. 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Based on this comparison the limitations of the energy sink stability criteria are identified."]},{"key":"dc:title","label":"Title","values":["The effects of liquid propellant motion on the attitude stability of spin stabilized space-craft"]}]}],"canonical_facts":{"dc:contributor.advisor":["Agrawal, Brij N."],"dc:contributor.department":["Department of Aeronautics and Astronautics"],"dc:creator":["Myers, Jack W. Jr."],"dc:date":["March 1990"],"dc:date.accessioned":["2013-11-20T23:33:39Z"],"dc:date.available":["2013-11-20T23:33:39Z"],"dc:date.issued":["1990-03"],"dc:description.abstract":["An analysis of the effects of liquid motion on the attitude stability of spin stabilized spacecraft is presented. The effects of varying the fuel load and the asymmetry of the platform are emphasized. The energy sink stability criteria are compared to the results of a computer simulation. 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