发明名称 Launch tube closure
摘要 A closure for a missile launch tube comprising frangible glass ribs mounted on a support ring of the tube to form a dome shaped closure. The ribs are joined to one another externally of and on the longitudinal axis of the launch tube, and a plastic or polymeric cover is mounted on and encloses the glass ribs. The external surface of the plastic cover is provided with a linear-shaped explosive charge and detonator. When the missile begins to move in the launch tube, the detonator is fired to detonate the linear-shaped explosive charge which cuts the plastic and fragments the glass ribs into small granules. The missile may then exit the launch tube without obstruction.
申请公布号 US4301708(A) 申请公布日期 1981.11.24
申请号 US19790060536 申请日期 1979.07.25
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY 发明人 MUSSEY, RICHARD A.
分类号 F41F3/077;(IPC1-7):F41F3/04 主分类号 F41F3/077
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