[i-2] Thermal Design

[2023-i-05] The On-orbit Demonstration and the Evaluation of the Thermal Mathematical Models in Multiple Missions of CubeSats Using the Same Bus System

*Yuki Kusano¹, Shingo Nishimoto¹, Kazuki Takashima¹, Kazuki Toma¹, Toshihiro Shibukawa¹, Shinichi Yokobori¹, Satoshi Ikari¹, Yoshihisa Shimada², Hajime Arai², Hirokazu Nakamura², Akihiro Ishikawa¹, Shuhei Matsushita¹, Ryu Funase¹, Shinichi Nakasuka¹ (1. The University of Tokyo, 2. Seiren Co., Ltd.)

Keywords:CubeSats, Thermal Design, Thermal Mathematical Model, Lessons Learned