FIELD: space engineering. SUBSTANCE: forming the orbital group is achieved by setting the positions of satellites on rocket and selecting the direction of rates of their separation, as well as by definite turn of rocket and stabilization of it in this position at moment of simultaneous separation of satellites. Collision of satellites in the course of separation is excluded due to proper organization of motion whose trajectories in zone of dangerous motion depend on rigid kinematic linkage of satellites with rocket and simultaneous operation of separation units. EFFECT: enhanced reliability. 2 cl, 5 dwg
