发明名称 PROJECTILE WITH STING FOR REDUCING DRAG
摘要 A rearwardly extending axial protuberance, known as a "sting," is secured to the base of a conventional projectile, such as a bullet or an artillery shell. The sting may assume a variety of configurations, such as cylindrical, frusto-conical, or combinations thereof, and can be utilized as a modification to be added to conventional projectiles, or can be fabricated as an integral part of a new series of projectiles. The sting causes a reduction in base pressure drag and thus lowers the rate of energy loss of the projectile in flight. Such reduction in drag increases the effective range of a bullet by enabling same to maintain a flatter trajectory; a comparable reduction in drag increases the maximum range of an artillery shell.
申请公布号 US3809339(A) 申请公布日期 1974.05.07
申请号 US19720243313 申请日期 1972.04.12
申请人 SIELING W,US;ZIESSE N,US 发明人 SIELING W,US;ZIESSE N,US
分类号 F42B10/42;F42B10/44;(IPC1-7):F42B13/02 主分类号 F42B10/42
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