@inproceedings{oai:jaxa.repo.nii.ac.jp:00016712,
 author = {菊池, 康介 and 清水, 克也 and 松田, 淳 and 佐宗, 章弘 and Kikuchi, Kosuke and Shimizu, Katsuya and Matsuda, Atsushi and Sasoh, Akihiro},
 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), A squared cross section ballistic range has been developed. It prevents flying objects to roll in the tube. It consists of a highpressure chamber (1.5 m), acceleration tubes (3 m), a ventilation tube (1.8 m), a launching tube (1.4 m), and a test chamber (3.2 m). At the ventilation tube, the precursor shock wave that is generated by the sabot when it passes through the acceleration tube and the driver gas are vented. At the launching tube, only the sabot affected by fore shock wave pressure that cause decelerating. On the other hand, the drag to the projectile is negligible. Therefore, projectile is separated from sabot in the launching tube. With this ballistic range, supersonic flight experiment of various shapes projectiles have been conducted., 形態: カラー図版あり, 資料番号: AA0064292019},
 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 = {ローリングのない三次元物体飛行や編隊飛行が可能なバリスティックレンジの開発},
 volume = {平成20年度},
 year = {2009}
}