| 摘要 |
A solar battery of a spacecraft comprises several panels, which are serially connected by attachment points to each other, a first panel is equipped with attachment points to the side wall of spacecraft, the panels are pivotally connected and in the folded position are pressed against the side walls of spacecraft. The battery is equipped with the attachment points of panels to the spacecraft panels in folded position, the attachment points are made in the form of rods firmly attached from the both sides of the panels, the attachment points of intermediate panels are made in the form of brackets installed on the side wall of spacecraft, and the attachment point of the end panel is made in the form of a profiled support, which is fastened on the outer side of end panel, and in the folded position is in contact with the end bracket equipped with a lock, and the rods and lock are made of a material, which has the property of thermo-mechanical shape memory. |
