Open AccessSimulating a triangular tube of a spacecraft solar array
Author(s) -
В. А. Нестеров,
Артем Суханов,
F. K. Sin’kovsky,
Yu G Vygonskiy,
А. В. Кузовников,
В. А. Левко,
T V Strekaleva
Publication year - 2019
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1399/4/044046
Subject(s) - spacecraft , tube (container) , stiffness , buckling , materials science , structural engineering , rib cage , fiber , aerospace engineering , engineering , composite material
The static analysis of anisogrid carbon-fiber triangular tubes is considered in the article. According to the minimum deformability, the optimum values of winding angles of the side ribs are determined. Buckling and stiffness analyses are included as well.