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Title Armature design for coaxial induction launchers
Creator/Author Andrews, J.A. ; Devine, J.R. (Texas Univ., Austin, TX (United States). Center for Electromechanics)
Publication Date1991 Jan 01
OSTI IdentifierOSTI ID: 5522050
Report Number(s)CONF-9004136--
Other Number(s)ISSN0018-9464; CODEN: IEMGA
Resource TypeConference
Specific TypeJournal Article
Resource RelationIEEE Transactions on Magnetics (Institute of Electrical and Electronics Engineers) ; Vol/Issue: 27:1; 5. IEEE symposium on electromagnetic launcher technology; 1-5 Apr 1990; Destin, FL (United States); DOE Project
Subject700460 -- Fusion Technology-- Heating & Fueling Systems; Fuels-- (1992) ;430100 -- Particle Accelerators-- Design, Development, & Operation; ARMATURES-- DESIGN;PLASMA GUNS-- A CODES;PLASMA GUNS-- T CODES; ACCELERATORS;ALUMINIUM;COMPUTER CODES;ELECTROMAGNETIC RADIATION;ELECTROMECHANICS;FINITE ELEMENT METHOD;INDUCTION GENERATORS;MATERIALS TESTING;PERFORMANCE TESTING;PLASMA ACCELERATION;REACTOR COMPONENTS
Related SubjectACCELERATION;COMPUTER CODES;ELECTRIC GENERATORS;ELEMENTS;MECHANICS;METALS;NUMERICAL SOLUTION;RADIATIONS;TESTING
Description/Abstract This paper reports on the armature design for a coaxial induction launcher that is influenced by a large set of highly coupled parameters.^The simplifying assumptions often employed in coaxial accelerator analysis, such as a uniform or sinusoidal axial distribution of the azimuthal armature current, are unrealistic in induction launchers with monolithic single-turn armatures.^In order to better understand the true dynamic behavior of coaxial accelerators, the Center for Electromechanics at The University of Texas at Austin (CEM-UT) has developed series of computer codes based on the current filament method.^By utilizing these performance codes in conjunction with electromagnetic (EM) and mechanical finite element programs, it is now possible to design high performance induction launchers with armatures that can withstand the considerable mechanical and thermal loads inherent in a coaxial accelerator launch.
Country of PublicationUnited States
LanguageEnglish
FormatPages: 639-643
System Entry Date2001 May 13

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