where E is Young's modulus for the rail, I is moment of inertia for the rail, k is foundation modulus for the support, ρ is density for the rail and A is the cross-sectional area of the rail. The launcher is configured such that the critical velocity increases along the axial direction towards the muzzle. In particular, a material term √E/ρ of the rail increases along the axial direction, such for the rail being made from a first material being proximate to the breech and a second material being proximate to the muzzle, such that the material term √E/ρ of the second material being greater than that of the first material. Alternatively, the rail is made into a first shape being proximate to the breech and a second shape being proximate to the muzzle, such that a shape term √I/A of the second shape is greater than that of the first shape."/>
公开/公告号US7409900B1
专利类型
公开/公告日2008-08-12
原文格式PDF
申请/专利号US20060602438
申请日2006-11-02
分类号F41B6/00;F41F1/00;
国家 US
入库时间 2022-08-21 20:12:56