Abstract
The optimal design of the skeleton panel of the solar panels of the spacecraft was designed taking into account the increased physical and mechanical characteristics through the use of composite materials and the method of topological shape optimization.
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CITATION STYLE
APA
Mirzaev, M. A., Smirnov, I. G., Dyshekov, A. I., Slavkina, V. E., Shereuzhev, M. A., & Aliev, S. A. (2020). Design of the solar panel frame of the spacecraft by 3D printing with composite materials. In IOP Conference Series: Materials Science and Engineering (Vol. 747). Institute of Physics Publishing. https://doi.org/10.1088/1757-899X/747/1/012009
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