Author:
Khaliulin V I,Batrakov V V,Savitskiy V V
Abstract
Abstract
The paper presents the results of research dedicated to design and development of spacecraft structures using radial braiding and transfer molding. Experience in development, optimization and manufacturing of structures with closed section and biaxial and triaxial reinforcement is described for bearing rod, X-fitting, support platform, transformable lattice structure and ‘capillary’ tube.
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