FIELD: aerospace technology.
SUBSTANCE: invention relates to spacecraft, and more specifically to nodes of sliding structures. The device for transforming spacecraft structures contains an unfolding axis on which two elements of the unfolding structure are fixed, fastened in the folded position with a latch. There is a bundle of elastically flexible carbon rods and two tubes rigidly fixed to the corresponding elements of the unfolding structure. One end of the bundle of elastic-flexible carbon rods is fixed in a tube fixed to one transformable element, and the other end of the bundle of elastic-flexible carbon rods is placed with the possibility of free movement inside the tube fixed to another transformable element.
EFFECT: simplification of the device is achieved.
6 cl, 2 dwg
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