• Home
  • Current congress
  • Public Website
  • My papers
  • root
  • browse
  • IAC-08
  • A6
  • 3
  • paper
  • effect of projectile shape on hypervelocity impact phenomenon

    Paper number

    IAC-08.A6.3.11

    Author

    Dr. Yosuke Nagao, JAXA, Japan

    Coauthor

    Mr. Takayuki Shimizu, Mitsubishi Heavy Industries Ltd., Jordan

    Coauthor

    Mr. Makoto Hikiji, Chugoku Kayaku Co., Ltd., Japan

    Coauthor

    Dr. Seishiro Kibe, Asian Institute of Technology, Thailand

    Coauthor

    Dr. Kenji Togami, Mitsubishi Heavy Industries, LTD, Japan

    Coauthor

    Mr. Hiroki Koinuma, Mitsubishi Heavy Industries, LTD, Japan

    Year

    2008

    Abstract
    The projectile of a 2 staged light gas gun has mostly spherical shapes. On the other hand, in the shaped charge system more accelerable to a high speed, it is checked also from the experiment of authors that the configuration of a jet is close to a hollow cylinder. So, in order to judge the test result using a shaped charge more exactly, the effect which the configuration of projectile has on breakage needs to be evaluated. Then, using a 2 staged-light gas gun which can change the configuration of projectile comparatively easily, the configuration similar to a shaped charge system was injected, and the check evaluated about the effect which a projectile configuration has on breakage was done. As a result, when the projectile from which only a configuration differs with the same mass at the same velocity to collide with a thick board, it turned out that there is no big difference in a breakage configuration. On the other hand, in the collision to a multiplex bumper configuration, it turned out that the effect which a projectile configuration has to a breakage configuration is great. This investigation shows the above check outline and a result. Moreover, the result evaluated about the validity of the method of a collision test to the bumper configuration using a shaped charge is shown.
    Abstract document

    IAC-08.A6.3.11.pdf

    Manuscript document

    IAC-08.A6.3.11.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.