FIELD: transport.
SUBSTANCE: invention relates to space engineering and can be used in withdrawable lattice structures. The transformable structure (TS) contains rigid supporting members, rigid flaps. Between supporting members, two pairs of flaps are located being pivotally connected with supporting members and with each other. Axes of rotation between supporting members and mating flaps lay in planes perpendicular to deployment direction, one axis includes at least two non-parallel to each other axes of rotation between flaps.
EFFECT: invention permits to improve reliability of deployment and rigidity of TS.
10 dwg
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