This report presents the results of an investigation of the effects of mass loss on the attitude behavior of spinning bodies in flight. The principal goal is to determine whether there arc circumstances under which the motion of variable mass systems can become unstable in the sense that their transverse angular velocities become unbounded.Obviously, results from a study if this kind would find immediate application in the aerospace field. "The first part of this study feann_s a complete and mathematically rigorous derivation of a set of equations that govern both the translational and rotational motions of general variable mass systems. The remainder of the study is then devoted to the application of the equations obtained to a systematic investigation of the effect of various mass loss scenarios on the dynamics of increasingly complex models of variable mass systems.It is found that mass loss can have a major impact on the dynamics of mechanical systems,includinga possiblechange in the systems stability picture.Factors such as nozzle geometry, combustion chamber geometry, propellant's initial shape, size and relative mass, and propellant location can all have important influences on the system's dynamic behavior. The relative importance of theseparameterson-system motion are quantified in a way thatisusefulfordesignpurposes.ii ACKNOWLEDGMENT