FIELD: aviation; rocket and space technology.
SUBSTANCE: invention relates to shell structures; it can be used in products of aviation and rocket and space technology. The adapter is a load-bearing rigid mesh structure made of spiral, annular, longitudinal ribs and frames, made of unidirectional polymer composite material. It has at least two support platforms for placing independent payloads (hereinafter – PL), inclined relatively to the support plane by 1-15° and fixed on identical conical shells of rotation with axes deflected by 30-60° from the central axis. The adapter does not require a separate support platform for the PL and the PL deflection mechanisms.
EFFECT: technical result is a reduction in the weight of the adapter, an increase in its strength, manufacturability and reliability of the design.
5 cl, 5 dwg
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