发明名称 System and method for shock isolation in a launch system
摘要 A projectile launching system includes a shock isolator 220 of at least three planar resilient support members defining a circumferential wall extending vertically between the projectile mounting frame 214 and a base portion 206. The shock isolator defines an opening through the isolator that provides for the uninterrupted flow of expelled rocket gases, as well as underside access to the projectile mounting frame. Each planar resilient support member forms an integral spring arrangement within the support member.
申请公布号 NZ601712(A) 申请公布日期 2014.08.29
申请号 NZ20110601712 申请日期 2011.03.01
申请人 LOCKHEED MARTIN CORPORATION 发明人 KALMS WILLIAM;ARORA TEJBIR;SNEDIKER JOHN
分类号 F41F3/00;F41F3/042 主分类号 F41F3/00
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