An MHD theory is developed for the standoff distance a, of the bow shock and the thickness Delta(ms) of the magnetosheath, using the empirical Spreiter et al. relation Delta(ms) = kX and the MHD density ratio X across the shock. The theory includes as special cases the well-known gasdynamic theory and associated phenomenological MHD-like models for Delta(ms) and a(s). In general, however, MHD effects produce major differences from previous models, especially at low Alfven (M(A)) and sonic (M(S)) Mach numbers. The magnetic field orientation, M(A), M(S), and the ratio of specific heats gamma are all important variables of the theory. In contrast, the fast mode Mach number need play no direct role. Three principal conclusions are reached. First, the gasdynamic and phenomenological models miss important dependances on field orientation and M(S) and generally provide poor approximations to the MHD results. Second, changes in field orientation and M(S) are predicted to cause factor of similar to 4 changes in Delta(ms) at low M(A). These effects should be important when predicting the shock's location or calculating gamma from observations. Third, using Spreiter et al.'s value for k in the MHD theory leads to maximum a(s), values at low M(A) and nominal M(S) that are much smaller than observations and MHD simulations require. Resolving this problem requires either the modified Spreiter-like relation and larger K found in recent MHD simulations and/or a breakdown in the Spreiter-like relation at very low M(A).
