FIELD: astronautics.
SUBSTANCE: invention relates to power structures of housings (PSH) of mesh structure, containing sling (cables) for fixation of spacecraft elements (for example, fuel tanks). Inner part of the proposed assembly is formed by platform (1) with slings (14) fixed between inner (2) and external (3) straps by means of bracket (4) with eye (7), washers (6) and nuts (5). Two bracket supports (12, 11) for installation respectively on internal and external sides of PSH (15) are interconnected by screws (13), forming external part of assembly. Said parts of the assembly are connected to each other by means of pin (8), washer (10) and nut (9). Bracket support sides repeat PSH ribs direction.
EFFECT: increased accuracy of adjustment (provision of uniform) tension of slings, reduced weight and unification of the assembly.
1 cl, 4 dwg
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Authors
Dates
2019-06-14—Published
2018-02-13—Filed