Host: The Japan Society of Mechanical Engineers
Name : Dynamics and Design Conference 2018
Date : August 28, 2018 - August 31, 2018
A novel composite structure arm for astronautical development by using CFRP and honeycomb core is already presented. In previous studies, the superiority of the presented arm is theoretically confirmed while experimental results possessed far below stiffness. The reason is estimated to be the failure in adhesion. To avoid this, solid shaping of the arm by using 3D printer is presented. In this study theoretical and experimental evaluation of the presented arm is carried out and their difference are examined.-
