公开(公告)号：WO2008102069A2

公开(公告)日：2008-08-28

申请号：PCT/FR2007002142

申请日：2007-12-20

Applicant: ATELIERS MECANIQUES DE PONT SU ,  MARTIN CHRISTIAN

Inventor： MARTIN CHRISTIAN

IPC: F42B15/01

CPC classification number: F42B15/01

Abstract: The invention relates to a guided missile (1) comprising: a body (10) with a generally cylindrical shape ending at the front in a cone-shaped nose (20); and a cylindrical sleeve (30) for mounting a NATO-standard guiding system at the front of the body; characterised in that the nose (20) includes a cylindrical connection portion (25) on which the sleeve (30) is attached.

Abstract translation: 本发明涉及一种导弹（1），包括：主体（10），其具有大致圆柱形的形状，其终端于锥形鼻（20）的前部; 以及用于在身体前部安装北约标准导向系统的圆柱形套筒（30） 其特征在于，所述鼻部（20）包括圆柱形连接部分（25），所述套筒（30）附接在所述圆柱形连接部分上。

公开(公告)号：WO2008102069A3

公开(公告)日：2008-10-30

申请号：PCT/FR2007002142

申请日：2007-12-20

Applicant: ATELIERS MECANIQUES DE PONT SU ,  MARTIN CHRISTIAN

Inventor： MARTIN CHRISTIAN

IPC: F42B15/01

CPC classification number: F42B15/01

Abstract: The invention relates to a guided missile (1) comprising: a body (10) with a generally cylindrical shape ending at the front in a cone-shaped nose (20); and a cylindrical sleeve (30) for mounting a NATO-standard guiding system at the front of the body, the nose (20) including a cylindrical connection portion (25) on which the sleeve (30) is attached. The cylindrical connection portion (25) is disposed between a front cone-shaped part and a rear cone-shaped part (23) of the nose and connects said two parts in a continuous manner.

Abstract translation: 本发明涉及一种导弹（1），包括：主体（10），其具有大致圆柱形的形状，其末端在锥形鼻部（20）中; 以及用于在身体前部安装NATO标准引导系统的圆柱形套筒（30），所述鼻部（20）包括圆柱形连接部分（25），所述套筒（30）附接在所述圆柱形连接部分上。 圆筒形连接部分（25）设置在前锥形部分和鼻部的后锥形部分（23）之间，并以连续的方式连接所述两部分。