FIELD: space technology.
SUBSTANCE: invention relates to space technology, is a payload module (PM) of a spacecraft and can be used to create a modular type SC for various purposes. SC PM consists of a base panel and a base panel of the second tier, two support panels and two dashboards. A cylindrical structure is installed on the base panel. The base panel of the second tier has a central opening that encloses the cylindrical structure. Support panels are located between the base panel and the base panel of the second tier. The base panel of the third tier is installed at the end of the cylindrical structure.
EFFECT: possibility of placing additional attachments and devices is achieved by increasing the rigidity of the structure and introducing an additional base panel.
1 cl, 2 dwg
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