主催: 一般社団法人 日本機械学会
会議名: 第29回 設計工学・システム部門講演会
開催日: 2019/09/25 - 2019/09/27
Multiobjective design optimization of the engine of the atmosphere-assisted reusable sounding rocket is performed for maximizing the maximum altitude and the payload weight. The result shows that a trade-off between maximization of maximum altitude and payload weight maximization.