Ammunition and explosives – Projectiles – Composite
Patent
1993-07-13
1995-05-09
Tudor, Harold J.
Ammunition and explosives
Projectiles
Composite
102703, F42B 1406
Patent
active
054130492
ABSTRACT:
The terminal effectiveness of fin stabilized, subcaliber armor piercing projectiles depends primarily on the impact velocity at the target. The aerodynamic drag and related velocity decay experienced over the trajectory from the gun to target is reduced by shortening the length of the acceleration transfer interface between subcaliber projectile and discarding sabot. This applies for multiple annular grooves and helical grooves. Special groove configurations to reduce the pressure drag and related boundary layer shock wave interaction are disclosed. The reduction in length of the acceleration transmitting interface permits its location to a position aft of the point of boundary layer transition from laminar to turbulent flow and therewith to take advantage of the low frictional coefficient of the laminar boundary layer over a large portion of the subcaliber projectile. The resulting reduction in aerodynamic drag is particularly effective for mid caliber projectiles.
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Christenson Craig
Feldmann Fritz K.
Griffith Paul J.
Pacific Armatechnica Corporation
Tudor Harold J.
Walsh Patrick J.
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