FIELD: aircraft engineering.
SUBSTANCE: invention relates to attachment of spacecraft hardware at its load-bearing structure made of polymer composites. This assembly consists of fastening and bearing straps secured with load-bearing structure element. Straps are interconnected, their guide faces being inclined at the angle aligned with that of load-bearing structure ribs. Bearing strap rests on the load-bearing structure crosshair to secure said fastening strap that makes the spacecraft hardware location surface and fixing point.
EFFECT: accurate positioning of hardware, ruled out destructive effects at cellular structure.
5 cl, 5 dwg
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