年次大会
Online ISSN : 2424-2667
ISSN-L : 2424-2667
セッションID: G191016
会議情報
G191016 一段式ガス銃の回転発射機構の検討及び基礎実験([G191]宇宙工学部門,一般セッション)
稲尾 大介波多 英寛藤原 和人川島 扶美子大谷 佳央
著者情報
会議録・要旨集 フリー

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抄録
The high-speed collision experiment is conducted,by the issue of space debris collision.However,the experiment in consideration of the influence of the rotation projectile is not carried out very much.The purpose of this study is to develop the single-stage gas gun which can fire a rotation projectile at low velocity.Improve a launching device and measure a turn and the velocity of the projectile with a high-speed video camera.The number of revolutions of the motor which turned a projectile used 14000rpm.The experimental conditions were being press gas,the length of the launch tube and pressure of vacuum chamber,raised the pressure of the pressure vessel,and it was found to be effective for projectilerotary maintenance to make an acceleration pipe a vacuum.The maximum number of turns of a projectile comprising this rotary launching device is 10000rpm.
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