Open AccessDevelopment of carbon/epoxy composite bracket for housing sensitive element of spacecraft
Author(s) -
В. А. Комаров,
А. А. Павлов,
С. А. Павлова
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/683/1/012088
Subject(s) - bracket , airframe , epoxy , spacecraft , composite number , structural engineering , carbon fibers , finite element method , structural element , materials science , element (criminal law) , composite material , computer science , engineering , aerospace engineering , political science , law
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.