Takaya Nakamura, Tatsuya Yamagami, Naoki Sekiya, Hiroshi Mizoguchi, Koji Tanaka
Proceedings of the International Astronautical Congress, IAC 2020-October 2020年
We are studying and developing a hybrid system combined with thin film and bulk structure to realize a solar power satellite (SPS). One of the problems of realization for SPS is the number of space transportation. Therefore, to reduce the number of space transportation, we're considering replacing some functions from a bulk structure with by lightweight and thin flexible structure. Also, to meet temperature requirements, thermal design of hybrid structure for the SPS should be considered. In this study, we found thermal structural conditions of hybrid system combined with thin film and bulk structure for SPS.