发明授权
- 专利标题: Special purpose firearms projectile
- 专利标题(中): 特殊目的火箭项目
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申请号: US3672304D申请日: 1970-03-30
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公开(公告)号: US3672304A公开(公告)日: 1972-06-27
- 发明人: ROGERS PATRICK F , HENDRICKSON WARREN L
- 申请人: LOCKHEED AIRCRAFT CORP
- 专利权人: Lockheed Aircraft Corp
- 当前专利权人: Lockheed Aircraft Corp
- 优先权: US2382570 1970-03-30
- 主分类号: F42B10/38
- IPC分类号: F42B10/38 ; F42B10/42 ; F42B11/02
摘要:
A small arms bullet with controlled flight characteristics fireable at high velocities from conventional small arms. The bullet has a projecting spike tip forming a supersonic shock wave cone. The bullet travels inside this shock wave cone and has low aerodynamic drag at supersonic velocities. The bullet is light weight and has a blunt drag face providing a high aerodynamic drag configuration for the bullet at subsonic flight velocities to rapidly decelerate the bullet after a preselected initial combat range, thereby reducing its long range danger to bystanders and property. Within the preselected combat range the shape and velocity characteristics of the bullet provide high ''''stopping power'''' yet a reduced lethality.
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