FIELD: cosmonautics.
SUBSTANCE: invention relates to space equipment, more specifically, to a spacecraft service systems module (SC SSM). The SC SSM consists of a central power unit made in form of a mesh cylindrical structure and panels. There are two additional control panels in the XOZ plane with units for attachment with the base panel and the top panel. The length of the additional control panels is not greater than the length of the base panel and the top panel. Support panels are installed parallel to the additional control panels, covering the perimeter of the rectangular parallelepiped in the XOZ plane, with units for attachment with the base panel, the top panel and the control panels. Accumulator battery panels are installed inside the control panels and connected with said panels and with the top panel.
EFFECT: increased structural rigidity is achieved.
1 cl, 2 dwg
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