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Abstract
The article considers the challenge of using layered carbon/epoxy composite materials in a high-loaded airframe structures. It is demonstrated by a redesign of the bracket for housing a sensitive element of the spacecraft. The new design approach considering simultaneously structural and technological features of composite constructions. It can also be applied to other design tasks to develop a structure of minimum weight.
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Details
1 Aircraft Design Department, Samara University, 34, Moskovskoye shosse, Samara, Russian Federation