@inproceedings{oai:jaxa.repo.nii.ac.jp:00004376,
 author = {牧野, 好和 and 冨田, 博史 and 本田, 雅久 and 橋本, 敦 and Makino, Yoshikazu and Tomita, Hiroshi and Honda, Masahisa and Hashimoto, Atsushi},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, Test conditioions for the first phase of JAXA's low-sonic-boom concept demonstration project(D-SEND#1) are considered. The purposes of the D-SEND#1 project are to validate the airbone sonic-boom measurement method and to make sure the possibillty of low-sonic-boom concept demonstration with the scaled airplane model by dive maneuver in D-SEND#2 project. For these purposes, the differences of sonic-boom signatures from two D-SEND#1 models have to be observed in the sonic-boom data measured with the airbone boom measurement system. The test conditions of D-SEND#1 drop test such as required altitude and position for the model separation, and atmospheric conditions, are defined through the sonic-boom propagation analyses of two D-SEND#1 models. These conditions are revised after the first drop test of D-SEND#1 conducted in May, 2011 at Sweden., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207004, レポート番号: JAXA-SP-11-015},
 pages = {21--26},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {低ソニックブーム設計概念実証落下試験(D-SEND#1)の試験実施条件検討},
 volume = {JAXA-SP-11-015},
 year = {2012}
}