2 papers
eess.SY2026
System Analysis and Pre-Flight Evaluation of Deployable Solar Panels for 3U CubeSat HOKUSHIN-1
Yuji Sakamoto, Masaki Aoi, Sho Suzuki +8
This paper describes the system design methodology derived from the development and evaluation tests of deployable solar panels to be mounted on a 3U CubeSat. The study mainly incl…
eess.SY2026
Lessons Learned from Structural Design and Vibration Testing of 50-kg Microsatellites Deployed from the International Space Station
Yuji Sakamoto, Junichi Kurihara, Shinya Fujita +2
Hokkaido University and Tohoku University have been developing and operating a constellation of 50-cm-class microsatellites for Earth observation. DIWATA-1, launched in 2016, was d…