Determination of mass-geometric characteristics of ballistic aircraft

An approach to determine the mass-geometric characteristics of the elements of the ballistic flight vehicle. It is shown that for the determination of all massgeometric characteristics of the two elements are needed maximum of three cycles of measuring the massgeometric characteristics of the ballistic flight vehicle as a whole. Proposed the problem of calculating the orientation of the elements of the ballistic flight vehicle that meets the requirements of the design documentation to the massgeometric characteristics of the flight vehicle. An approach to its solution.