Аннотация:Low-cost interplanetary tours with the high inclined orbit's formation in the Solar system with use of gravitational maneuvers near its planets (Earth and Ve-nus) and with the accurate ephemeris using are considered. Limited dynamic opportunities of their use require multiple passes near them. Topicality of the regular creation of optimum scenarios – sequences of cranking passing of celestial bodies and the solution of conditions of their execution is obvious. This work is devoted to the description of required features of trajectory's beams for the creation of such chains. Previously a comparative analysis of various modern astrodynamics studies of the 3D implementation of GAMs taking into account accurate ephemerides was performed. Improved analytical formulas for the change of inclination of an SC orbit as a result of 3D GAMs were obtained and realistic results of the computation of parameters of the SC orbit inclination changes at the planets of the Solar system and their moons were presented. In this paper, we describe algorithms for designing multi-pass chains of GAMs that result in an energy-efficient increase of the inclination of the SC orbit to the ecliptic plane. Simultaneously, a generalization of the analytical formulas for the general case of elliptic orbits of the SC and the partner planet for the GAM is obtained. Applications of its using for the study of concrete options of mission "InterhelioZond" are given.