Inverse solution existence and uniqueness issues are discussed for superson
ic and hypersonic three-dimensional inverse procedures that use space-march
ing techniques. By using extreme body-slope angle, a simple method to estim
ate the limiting domain of inverse solution existence is proposed and appli
ed to several example test cases with and without angle of attack. The meth
od provides useful information about possible target pressure distributions
and inverse solution existence without performing any inverse calculations
. By investigating the relations between the surface pressure and the body
geometry, a general explanation for inverse solution uniqueness has been de
scribed, sample calculations to support this explanation are presented.