FIELD: astronautics.
SUBSTANCE: invention relates to power structures for installation, in particular, on-board spacecraft of various equipment by means of cables. Interface consists of frame with a set of holes for its attachment to mounting elements of different configuration. On the outside of the frame there installed are units for tension adjustment of the cables, and on the inner side – fixing units. Between these assemblies there is a pad with fixing ropes attached to the equipment. Units of tension adjustment are detachable, and assemblies of fixation are stationary. All assemblies are equipped with required fasteners: spherical washers, pins, nuts, etc.
EFFECT: improved manufacturability of tension adjustment assemblies, reduced weight and unification of the interface.
1 cl, 1 dwg
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