HIGHLIGHTS
- who: Yutaro Furuichi and collaborators from the Department of Aeronautics and Astronautics, Tokyo Metropolitan University, Hino, Tokyo, Japan have published the Article: Numerical Study of the Magnetic Damping Effect on the Sloshing of Liquid Oxygen in Propellant Tank, in the Journal: (JOURNAL)
- what: Considering the most dangerous situation on the attitude of the spacecraft, the authors focused on the case that the initial liquid phase was located in the lower half of the tank under the impact force excited from the lateral direction.
- how: In this study aiming at damping the sloshing without . . .
If you want to have access to all the content you need to log in!
Thanks :)
If you don't have an account, you can create one here.