主催: 一般社団法人 日本機械学会
会議名: 第26回スペース・エンジニアリング・コンファレンス
開催日: 2017/12/22 - 2017/12/23
Deployable structures are necessary for spacecraft to challenge advanced missions. It is important in designing the deployable space structures that they are easily deployable and reliably repeatable. The buckling in some cases enables external impetus to deploy the structure to be smaller, and enables stable deployment. The paper proposes a new available deployable structure “Deployable Cube”, which applies buckling actively.