Satellite deployment structure

摘要

In a solar array paddle having a plurality of panels which are connected to a main body of a satellite and rotatably connected to one another, a plurality of elastic insertion member for prevention of vibration is disposed in a clearance between each of the panels and in that between the main body and the panel adjacent to the main body when the panels are housed with them folded and layered. Each of the insertion member for prevention of vibration is inserted into the above-described clearances and those between the main body of the satellite and the panels adjacent to the main body such that one surface thereof is contacted with a relevant surface and the other surface thereof is adhered to another relevant surface.