FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly, to spacecraft payload modules (SC PLM). SC PLM is installed on the spacecraft central part. It consists of two support panel structures, which serve for their fixation on central part of SC and for arrangement of two instrument panels and two base panels connected by orthogonal panels. Part of orthogonal panels form a closed structure with a base in the form of a polyhedron. Another part of orthogonal panels is rigidly attached to outer edges of closed structure. Above elements are located within the limits of the base panel perimeter.
EFFECT: higher rigidity of structure.
1 cl, 2 dwg
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Authors
Dates
2020-08-04—Published
2019-12-20—Filed