@inproceedings{oai:jaxa.repo.nii.ac.jp:00003838,
 author = {下田, 孝幸 and 山田, 和彦 and 高橋, 裕介 and Shimoda, Takayuki and Yamada, Kazuhiko and Takahashi, Yusuke},
 book = {宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, JAXA Sagamihara Arc wind tunnel was established as 1MW high power arc tunnel in 1996. It had contributed to the development of “HAYABUSA” capsule successfully and “HAYABUSA2” which will be launched in this year. After “HAYABUSA2,” the exploration to Jupiter orbit is planned. The returned capsule of the vehicle will be exposed heat flux of over 30MW/m2. Sagamihara Arc tunnel is preparing to update the performance to develop the highly heat resistant material for the recovery to the earth. The wind tunnel also started its activity as Inter-University Research facility in 2014. The heat flux and other physical characteristics are under re-investigation and identification for stable operation. We report the results of them so far., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023003, レポート番号: JAXA-SP-14-010},
 pages = {13--16},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {JAXA相模原アーク風洞の特性評価},
 volume = {JAXA-SP-14-010},
 year = {2015}
}