FIELD: space engineering. SUBSTANCE: proposed system is used for satellite, personnel, cargo unit of orbital station. Proposed suspension system includes one or more hydraulic chambers of variable geometry which are arranged between launch vehicle and payload. Provision is made for first and second rigid members secured to chamber and payload on one side and to launch vehicle on other side for transmission of arising loads through structure of said chamber. Hydraulic chamber and said rigid members are circular in shape; each first and second member has at least one external and one internal fin which are separated by said chamber. Various versions of hydraulic chambers, their members and structural beams are described in invention. EFFECT: reduction of mass; avoidance of transmission of peak loads, impact loads or vibrations to payload. 16 cl, 12 dwg
