发明名称 Pressure limiting missile launching system
摘要 The system consists of a launch tube (10) contg. the projectile (12) and its propulsive charge (14), which is associated with a pressure limiter (18), designed to compress when the charge is detonated. The pressure limiter can be made from a friable material such as: (a) a plastic foam; (b) a metal or plastic honeycomb structure, between two skins of laminated carbon or glass fibres and epoxy resin; and (c) hollow metal balls or metal tubes, esp. of Al, which buckle on compression. The propulsive charge (14) is associated with a moving breech, consisting of a charge or an ejectable and dispersible counterweight (16), with the compression limiter (18) located between it and the propulsive charge.
申请公布号 FR2720821(A1) 申请公布日期 1995.12.08
申请号 FR19940006957 申请日期 1994.06.07
申请人 SERAT 发明人 PORTRAT JEAN-PIERRE
分类号 F41A1/10;F42B5/05;(IPC1-7):F41A1/00;F42B5/16 主分类号 F41A1/10
代理机构 代理人
主权项
地址