RETENTION OF LARGE flat design the spacecraft

摘要

Apparatus mounting large flat structures on a spacecraft, comprising a frame as a support structure rigidly secured to the spacecraft, the support nodes and communication nodes located on the power belts and provided with insulating spacers, characterized in that the axes intersection point of symmetry of the large flat structure such as radar antennas, there is a rigid connection with the frame of the radar antenna, the support assemblies arranged along the axes of symmetry of the radar en enny embodied as spring-loaded roller covered with forks fixed to the radar antenna, the rollers interact with the slots overlap, is rigidly fixed to the RLA, and communication centers located on the lines connecting the central RLA point with places of installation are designed as crank axle which interact with the rolling bearings contained in the casing, one of which is fixed to the frame and the other on the radar antenna.