@techreport{oai:jaxa.repo.nii.ac.jp:00002733,
 author = {鈴木, 広一 and 高嵜, 浩一 and 南, 吉紀 and 甲斐, 高志 and 佐藤, 哲也 and 小林, 弘明 and 藤田, 和央 and 伊藤, 健 and 黒滝, 卓司 and Suzuki, Hirokazu and Takasaki, Koichi and Minami, Yoshinori and Kai, Takashi and Sato, Tetsuya and Kobayashi, Hiroaki and Fujita, Kazuhisa and Ito, Takeshi and Kurotaki, Takuji},
 month = {Oct},
 note = {In this research, optimal design, evaluation, and aerodynamic problems for future space transportation systems are conducted. An optimal design program is developed in the research of optimal design and evaluation. The design criteria are also investigated and several types of the concept for the future space transportation systems are designed optically and are evaluated. In the last physical year, a developmental plan of prototype of the design program was established and a part of the prototype was developed. The catalysis and the real gas effect are dealt as aerodynamic problems for the future space transportation systems. In the last physical year, precious data were obtained by the high enthalpy wind tunnel., 資料番号: AA0047944002, レポート番号: JAXA-RM-04-009},
 title = {システム解析の研究:コンセプトスタディプログラムの開発と設計基準の検討および空力技術に関する研究},
 year = {2004}
}