Open AccessDesign and process for production of spacecraft structures using radial braiding and transfer molding
Author(s) -
V. I. Khaliulin,
В. В. Батраков,
V. V. Savitskiy
Publication year - 2019
Publication title -
iop conference series. materials science and engineering
Language(s) - English
Resource type - Journals
eISSN - 1757-899X
pISSN - 1757-8981
DOI - 10.1088/1757-899x/683/1/012058
Subject(s) - spacecraft , molding (decorative) , capillary action , mechanical engineering , materials science , transfer molding , tube (container) , engineering , computer science , aerospace engineering , mold , composite material
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.