Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : December 17, 2020 - December 18, 2020
In this study, I will propose a deployable cubic structure called Jackson Cube, which is based on origami. The size is 10cm x 10cm x 1cm when stored and it deployed 1U. This structure has two advantages. First, it can mount on CubeSat, because it has square cross section. Second, it can combine several structures to form the large structure. I conducted the vibration tests to investigate the stiffness and deformation modes of a deployable structure. I compared the results with the PSDs obtained from the structural analysis. Finally, I discussed the difference of structural analysis and vibration test.
