@inproceedings{oai:jaxa.repo.nii.ac.jp:00007678,
 author = {四宮, 康雄 and 松本, 甲太郎 and 星野, 健 and 松藤, 幸男 and Shinomiya, Yasuo and Matsumoto, Kotaro and Hoshino, Takeshi and Matsufuji, Yukio},
 book = {平成16年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {月の表面温度は昼夜で激しく異なり、赤道付近では、正午には120度Cまで上昇し、夜間には-180度Cまで下がる。そこで、現有機器の低温耐性はどの程度か、試験した。又、有限要素法の熱解析ソフトであるANSYSを用いて、月面の熱数学モデルを作成し、レゴリスの温度応答を求めると共に、レゴリス上のローバの温度応答を求めた。, The moon surface temperature varies violently, such as 120 C at noon and - 180 C at night. In order to carry out the mission, night survival is the one of the most important issues. Since, super low temperature endurance test was performed to some devises. In addition, using the ANSYS, thermal analysis software of finite element method, temperature response of the lunar regolith and the rover was obtained., 資料番号: AA0047897045},
 pages = {259--264},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {Super low temperature endurance test and thermal analysis for night survival on moon},
 year = {2005}
}