发明名称 Locking assembly for a rocket and launch tube
摘要 A pair of locking members to releasably lock a rocket in a launch tube. Each locking member has a forward end engaging the rocket and a rear end engaging the tube. A retaining strut engages the two rear ends of the locking members to hold the locking members in locking engagement. When the rocket is fired, the exhaust from the rocket moves the retaining strut out of retaining engagement to permit leaf springs on the locking members to pivot the locking members out of locking engagement and permit the rocket to move out of the tube.
申请公布号 US4304170(A) 申请公布日期 1981.12.08
申请号 US19790030109 申请日期 1979.04.16
申请人 THE BOEING COMPANY 发明人 KING, DAVID W.
分类号 F41F3/052;(IPC1-7):F41F3/04 主分类号 F41F3/052
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