@article{oai:kyutech.repo.nii.ac.jp:00006070,
 author = {Masui, Hirokazu and 増井, 博一 and 世利, 祐樹 and Seri, Yuki and 濱田, 朗充 and Hamada, Akimitsu and Cho, Mengu and 趙, 孟佑},
 issue = {5},
 journal = {日本航空宇宙学会論文集, Journal Of the Japan Society for Aeronautical and Space Sciences},
 month = {Oct},
 note = {This paper describes the thermal design method of Horyu-2. Horyu-2 was developed by Kyushu Institute of Technology. The project started in 2010 and Horyu-2 was launched by H-2A of JAXA on May 18 2012. At present, Horyu-2 is carrying out many missions and transferring on-orbit data. Horyu-2 orbits 680 km with sun-synchronous polar orbit. Feature of Horyu-2 are lightweight (7.1kg) and large surface (30cm cube) compared with a conventional cube-sat. Thermal design is needed to keep the temperature within the safe range. We conducted thermal analysis in a step-by-step in each phase. This paper reviews the thermal design processes and discusses on-orbit data acquired after launch.},
 pages = {270--275},
 title = {超小型衛星「鳳龍弐号」の熱設計・検証手法と軌道データ解析},
 volume = {64},
 year = {2016},
 yomi = {マスイ, ヒロカズ and チヨウ, メンウ}
}