This technical memorandum describes a method for determining the transverse deflections of a uniformly loaded, thin circular plate of constant thickness supported by single or multiple rings of equally spaced discreet points. The rotations are assumed free at each point. This could have application in the design of telescope mirror supports that must minimize structural gravitational deformations. It could also be of general use to the structural analyst. Craig, L. D. and Boulet, J. A. M. Marshall Space Flight Center NASA/TM-1999-209631, NAS 1.15:209631, M-942