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dc.contributor.advisorScrivener, Sandra L.
dc.contributor.authorRaney, Elisa Anne.
dc.dateJune 1995
dc.date.accessioned2012-07-31T19:53:46Z
dc.date.available2012-07-31T19:53:46Z
dc.date.issued1995-06
dc.identifier.urihttps://hdl.handle.net/10945/7517
dc.description.abstractTopaz II is a Russian made nuclear powered satellite purchased by the United States. This thesis provides a vibration analysis of the power unit of Topaz II. Several experimental vibration tests were conducted on the actual power unit by Sandia National Laboratories, in Albuquerque, New Mexico. Utilizing Structural Dynamics Research Corporation's I-DEAS software, this model was tested using the same vibration test values as those performed on the actual power unit. The lateral and axial, experimental and theoretical, sine tests were then analyzed. The purpose of this analysis was to determine how accurate a representation the model was of the actual Topaz unit. This was accomplished through comparison of natural frequencies obtained experimentally with those predicted from I-DEAS testing of the finite element model. The frequency range of interest was from 0 Hz to 200 Hz. When solved for system modes, the model predicted all natural frequencies within 4.6 Hz of those found experimentally. The average variation between theoretical predicted and experimental determined natural frequencies was 1.8 Hz.en_US
dc.description.urihttp://archive.org/details/vibrationnalysis109457517
dc.format.extent185 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleVibration analysis of Topaz IIen_US
dc.typeThesisen_US
dc.contributor.departmentAstronautical Engineering
dc.description.serviceU.S. Navy (U.S.N.) author.en_US
etd.thesisdegree.nameM.S. in Astronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAstronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US


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