| 发明名称 |
SUPERSONIC PROJECTILE NOSE CONES WITH FLAT TIPS |
| 摘要 |
Supersonic projectile nose cones with flat tips are disclosed. An example apparatus includes a nose cone for a projectile configured for supersonic flight at velocities of at least Mach 2.0. The nose cone has an axisymmetric body extending from a base to a tip. The body has a thickness and defines an interior cavity. The tip is defined by a flat face normal to a central axis of the projectile. |
| 申请公布号 |
US2016252334(A1) |
申请公布日期 |
2016.09.01 |
| 申请号 |
US201414218069 |
申请日期 |
2014.03.18 |
| 申请人 |
The Boeing Company |
发明人 |
Cary Andrew W.;Dorgan Andrew J. |
| 分类号 |
F42B10/46;B64C1/00;B64C30/00 |
主分类号 |
F42B10/46 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus, comprising:
a nose cone for a projectile configured for supersonic flight at velocities of at least Mach 2.0, the nose cone having an axisymmetric body extending from a base to a tip, the body having a thickness and defining an interior cavity, and the tip being defined by a flat face normal to a central axis of the nose cone. |
| 地址 |
Chicago IL US |
