FIELD: mechanical engineering.
SUBSTANCE: invention relates to spacecraft equipment, more specifically to toroidal support structures and support units. The toroidal support structure comprises one or more lateral panels forming a tubular ring and one or more bottom panels forming a flat ring. These rings define the toroidal shape of the structure. Furthermore, the structure also comprises several insulating linear support components connected to the upper edge of the tubular ring, and a plurality of partitions. The toroidal support structure can be attached to different types of mounting bases, such as the cryogenic tank of the spacecraft.
EFFECT: achieved is the elimination of the structural transformation.
13 cl, 6 dwg
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