[C-2] Structural Dynamics and Control

[2022-c-07] Experimental Studies of Sloshing Dynamics for the Tank with Hemispheric Diaphragm

*Taro Kawano¹, Nobukatsu Okuizumi², Hikaru Eguchi³, Keisuke Michigami¹, Hitoshi Hamori¹, Susumu Yasuda¹, Rie Tagai¹, Shujiro Sawai² (1. Japan Aerospace Exploration Agency, Research and Development Directorate, 2. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, 3. Muroran Institute of Technology, Aerospace Plane Research Center)

Keywords:Sloshing, Diaphragm Tank, SLIM, Lander