@article{oai:jaxa.repo.nii.ac.jp:00022445,
 author = {杵淵, 紀世志 and 加納, 康仁 and 齊藤, 靖博 and 沖田, 耕一 and 姫野, 武洋 and Kinefuchi, Kiyoshi and Kano, Yasuhito and Saito, Yasuhiro and Okita, Koichi and Himeno, Takehiro},
 journal = {航空宇宙技術},
 month = {Aug},
 note = {For future space transportation system development, efficient liquid propellant acquisition technologies under microgravity could berequired to realize long-term missions in orbit. Microgravity environment is generally established through drop tower, parabolic flight by airplane ororbital/suborbital experiment. These methods are large-scale or not flexible so that compact and simple method is needed for the efficientdevelopment. To respond to such request, we propose a static experiment on the ground to realize the similar static free surface under microgravity.The ground experimental result was compared with the results of two types of two-phase flow simulation codes for the verification of themethodology and discuss the characteristics of these numerical codes. We also simulated the free surface under the actual flight condition by usingthe same simulation method and result showed the validity of the experimental method., 資料番号: PA1410086000},
 pages = {73--77},
 title = {微小重力下での液体推薬保持技術開発のための地上模擬実験},
 volume = {12},
 year = {2013}
}