@inproceedings{oai:jaxa.repo.nii.ac.jp:00016747,
 author = {高島, 康弘 and 笠原, 次郎 and 船木, 一幸 and Takashima, Yasuhiro and Kasahara, Jiro and Shepherd, Joseph E. and Funaki, Ikko},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), We investigate the dependence of the thrust increment on the amount of propellant in vacuum condition by using straight-extended shock tube hung in a ballistic pendulum arrangement in a vacuum chamber, instead of a single-cycle detonation tube, and also, using the method of characteristics. Initial pressure inside the tube was 0.86 MPa, whereas pressure inside the vacuum chamber was 400 Pa, and fill fraction between 19.8 % and 100 % were studied. The Impactor calibration and the error evaluation was carried out. The specific impulse increased most when length of the extension tube is 1.22 m (longest case) and we think that lower specific heat ratio driver gas or a longer extension tube can produce higher specific impulse., 形態: カラー図版あり, 資料番号: AA0064292054},
 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)},
 title = {衝撃波管にて生成される力積に関する研究},
 volume = {平成20年度},
 year = {2009}
}