- 著者
-
赤星 保浩
花田 俊也
田村 英樹
町田 裕
福重 進也
高良 隆男
- 出版者
- 一般社団法人 日本機械学会
- 雑誌
- 年次大会講演論文集
- 巻号頁・発行日
- vol.2006, pp.345-346, 2006
In order to simulate the debris impacts in geosynchronous orbit, we need the launcher that can launch the projectile under approximately 1[km/sec]. We converted a two-stage light gas gun into a powder gun. In generally, though sabot separation technique is used to launch the projectile of sphere, we can not apply its technique to a our powder gun. So we also conducted the development of new separation technique of projectile of sphere. In particular, we will show with the focus on the new separation technique.