@article{oai:jaxa.repo.nii.ac.jp:00033249,
 author = {佐宗, 章弘 and 大津, 広敬 and 安部, 隆士 and 澤田, 恵介 and 水野, 裕保 and Sasoh, Akihiro and Otsu, Hirotaka and Abe, Takashi and Sawada, Keisuke and Mizuno, Hiroyasu},
 journal = {The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule},
 month = {Mar},
 note = {An expansion tube has a unique capability of generating a hypervelocity flow without experiencing a stagnation condition of the test gas. Related to MUSES-C superorbital reentry flow condition, experimental and numerical simulations were conducted in domestic institutions as well as in University of Queensland, Australia. This paper summarizes the characteristics of the facility and results of their investigations., 資料番号: SA0200022000},
 pages = {165--176},
 title = {Utilization of Expansion Tube for MUSES-C Reentry Simulation},
 volume = {17},
 year = {2003}
}