Sabot assembly for a subcaliber spin stabilized projectile

• US 4,148,259 A
• Filed: 10/03/1977
• Issued: 04/10/1979
• Est. Priority Date: 10/03/1977
• Status: Expired due to Term

• Current Assignee: United States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
• Original Assignee: The United States Of America As Represented By The Secretary Of The Army
• Inventors: Yuhash, Ladd, Fischer, Gary W.
• Primary Examiner(s): Pendegrass, Verlin R.
• Application Number:
  US05/838,781
• Time in Patent Office: 554 Days
• Field of Search: 102/93, 102/DIG. 10
• US Class Current: 102/522
• CPC Class Codes: F42B 14/064 Sabots enclosing the rear end of a kinetic energy projectile, i.e. having a closed disk shaped obturator base and petals extending forward from said base

Abstract

A spherical convex pusher plate member is positioned intermediate the rear end of a subcaliber tubular projectile and the forward section of a cup shaped sabot carrier to improve the ballistic performance of the projectile by reduction of a parasitic weight and faster separation of the carrier after launch. Propellant gas pressures acting on the convex spherical section of the pusher plate causes deflection thereof sufficient to force the sabot to loosen from the projectile to provide an improvement in projectile velocity.

Claims

1. An apparatus for launching a spin stabilized hypervelocity subcaliber tubular projectile from a gun which comprises:

sabot means for obturating said subcaliber projectile passing through the barrel of said gun and for imparting rotation to said projectile which includes;

a cup shaped molded plastic housing having a spherical concave inner closed end therein; and

pusher plate means fixedly molded within said spherical concave inner closed end of said housing intermediate said sabot means and the rear end of said projectile for increasing the velocity of said projectile by reducing the parasitic weight of said pusher plate means, for aiding the removal of said means from said projectile after said projectile exits from the bore of said gun and for absorbing stress imposed on said sabot means and said projectile due to launch forces.

2. An apparatus for launching a spin stabilized subcaliber tubular projectile as recited in claim 1 wherein said pusher plate means comprises a spherical convex, plate having a central curved section, an inner spherical concave surface of said central curved section having a radius of curvature "r" and a convex spherical surface having a radius of curvature of "R", and a flat annular shoulder section integrally connected with said central curved section forming a plate having an outside diameter "D".

3. An apparatus as recited in claim 2 wherein said spherical convex plate is made of steel material.

4. An apparatus for launching a spin stabilized hypervelocity subcaliber tubular projectile from a gun which comprises:

sabot means for obturating said subcaliber projectile passing through the barrel of said gun and for imparting rotation to said projectile which includes;

a cup shaped molded plastic housing having a spherical concave inner closed end therein;

pusher plate means fixedly molded within said spherical concave inner closed end of said plastic housing and intermediate said sabot means and the rear end of said projectile for increasing the velocity of said projectile by reducing the parasitic weight of said pusher plate means, for aiding the removal of said means from said projectile after said projectile exits from the bore of said gun and for absorbing stress imposed on said sabot means and said projectile due to launch forces which includes;

a spherical convex plate having a central curved section, an inner spherical concave surface of said central curved section having a radius of curvature "d" and a convex spherical surface having a radius of curvature of "R", and a flat annular shoulder section integrally connected with said central curved section forming a plate having an outside diameter "D" wherein said spherical convex plate is made of steel having a cross-section thickness which allows said plate to deflect 0.1 inches when subjected to a propellant chamber pressure of 48,000 p.s.i., causing said outside diameter "D" of said plate to increase approximately 0.05 inches and aids in the removal of said sabot means for said projectile when said projectile exits from the bore of said gun.