[F-4] Mission Results and Lessons Learned

[2022-f-18] Revival and Successive Operation of 3U CubeSat OrigamiSat-1 with Multifunctional Deployable Membrane

*Shuhei Koike¹, Motoki Moritani¹, Misato Ishiwata¹ , Shinya Tamura¹, Kazuki Nagai¹, Hiraku Sakamoto¹, Hiroki Nakanishi¹, Hiroki Nakanishi¹, Takashi Tomura¹, Hiroshi Furuya¹, Akihito Watanabe² (1. Tokyo Institute of Technology, 2. Sakase Adtech, Co., Ltd.)

キーワード：CubeSat, Small satellite, Membrane structure, Gossamer spacecraft, Deployed shape