@inproceedings{oai:jaxa.repo.nii.ac.jp:00038829,
 author = {丹野, 英幸 and 小室., 智幸 and 永井, 大樹 and Tanno, Hideyuki and Komuro, Tomoyuki and Nagai, Daiki},
 book = {日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム, JSASS Northern Branch 2016 Annual Meeting and the 17th Symposiun on Propulsion System for Reusable Launch Vehicles},
 month = {Mar},
 note = {日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム（2016年3月9日-10日. 北海道大学大学院工学研究院), 札幌市, 北海道, A data reduction sceme was developed to evaluate aerodynamic stability of reentry capsule shaped projectiles under subsonic free-flight condition. The final goal of the work was to obtain benchmarks of stability characteristics to compare with wind tunnel test results or CFD calculations. A free-flight test campaign was conducted with an air driven single-stage gas gun in JAXA Kakuda Space Center. In the test campaign, a capsule shaped projectile of 380g mass and of 90 mm diameter launched at flight speed 110m/s. During 52meter free-flight, pitching motion of the projectile was measured with an onboard miniature data-logger and piezoelectric accelerometers in the projectile. Damping factor during free-flight was successfully obtained through the developed data reduction scheme. Nevertheless, aerodynamic stability of this projectile has not be determined due to lack of test data., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AC1600098000},
 publisher = {日本航空宇宙学会北部支部, Northern Branch of the Japan Society for Aeronautical and Space Sciences},
 title = {バリスティックレンジを用いたカプセル形状模型空力安定評価},
 volume = {17},
 year = {2016}
}