@inproceedings{oai:jaxa.repo.nii.ac.jp:00006618,
 author = {山本, 行光 and 吉田, 正廣 and 川戸, 博史 and Yamamoto, Yukimitsu and Yoshida, Masahiro and Kawato, Hiroshi},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {TSTO reusable launching system has come to be considered a main candidate for future space transport systems. Numerical simulation has played a very important role in the aerodynamic design of space transport vehicles such as HOPE-X and the related re-entry flight experiments. In the present report, recent studies of the aerodynamics of the several re-entry vehicles are introduced and the application of the multi-disciplinary simulation technology is described for the construction of future reusable TSTO space transport systems., 資料番号: AA0047427017, レポート番号: JAXA-SP-03-002},
 pages = {91--96},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {将来型再使用宇宙輸送システムに向けた空力数値シミュレーションの経過と今後の展望},
 volume = {JAXA-SP-03-002},
 year = {2004}
}