FIELD: aviation.
SUBSTANCE: power structure of the spacecraft platform is the carbon-plastic mesh structure in the form of the cylindrical tube, installed by one of its bases inside the rectangular parallelepiped coaxially with its axis. The parallelepiped consists of the panel-base and the top panel, connected to the cylindrical tube by means of the corners, and between each other by the support panels.
EFFECT: invention allows to achieve the structure unification, high strength characteristics, reducing of the platform weight, implementation of this technical solution allows to provide simultaneous launch of several devices.
4 dwg
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