Results will be presented of the testing to stress failure of a series
of small, 10 mm bore pulse magnets reinforced with different varietie
s and thicknesses of carbon composite. The field reached at failure al
lows a calculation of the stresses generated within the carbon fiber a
nd a consequent comparison with computer models of highly stressed com
posite reinforced magnets. Where necessary, empirical corrections can
be made in light of the experimental results. It will be shown that an
accurate estimation of the radial and axial elastic modulus of the co
mposite is of paramount importance in the modeling of stress transfer
throughout the shell. The future utility of composites will be discuss
ed together with an examination of the alternatives. (C) 1998 Elsevier
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