Dynamic instability reduced range round
A multi-piece projectile for a small arm training ammunition round maintains stable flight until reaching transonic speeds. During transonic and subsonic flight, aerodynamic features located on the projectile generate a pressure differential to increase limit cycle motion of the projectile. The aerodynamic features are located on a portion of the projectile which does not interface with rifling elements of the gun barrel and may include protrusions in or extrusions from the projectile.
1. A projectile for a small arms training ammunition round which comprises an aerodynamic feature located on an ogive of the projectile which does not interface with the rifling of a gun barrel and which generates a pressure differential which during transonic and subsonic flight increases the limit cycle motion of the projectile thereby causing the projectile to become dynamically unstable, wherein the aerodynamic feature comprises one or more radial cuts, said one or more radial cuts being defined by a first surface and a second surface, wherein the first surface comprises a flat surface extending radially outward from a central longitudinal axis of the projectile and the second surface comprises a curved surface intersecting with the first surface at a base edge.
2. The projectile of claim 1 wherein the one or more radial cuts are a predetermined cut distance from a cylindrical midsection determined by a barrel rifling diameter.
3. The projectile of claim 1 wherein the curved surface further comprises an outer edge comprising an arc and wherein an angle of a chord of the arc is within a range of eight degrees to twelve degrees.
4. The projectile of claim 1 wherein the arc is dimensioned such that an angle formed by a tangent line to the arc is less than or equal to ninety degrees with respect to a meplat of the projectile.
5. The projectile of claim 1 further comprising a semi-circular depression in a base of the projectile.
6. A multi-piece projectile for a small arm training ammunition round which comprises:
a main body;
a penetrator extending from the distal end of the main body, wherein the penetrator comprises a portion of an ogive; and
an aerodynamic feature located on the portion of the ogive located on the penetrator, wherein said portion of the ogive does not interface with a rifling of a gun barrel, wherein the aerodynamic feature generates a pressure differential which during transonic and subsonic flight increases the limit cycle motion of the projectile thereby causing the projectile to become dynamically unstable and wherein the aerodynamic feature comprises one or more radial cuts, said one or more radial cuts being defined by a first surface and a second surface, wherein the first surface comprises a flat surface extending radially outward from a central longitudinal axis of the projectile and the second surface comprises a curved surface intersecting with the first surface at a base edge.
7. The projectile of claim 6 wherein the one or more radial cuts are a predetermined cut distance from a cylindrical midsection determined by a barrel rifling diameter.
8. The projectile of claim 6 wherein the curved surface further comprises an outer edge comprising an arc and wherein an angle of a chord of the arc is within a range of nine degrees to ten degrees.
9. The projectile of claim 6 wherein the arc is dimensioned such that an angle formed by a tangent line to the arc is less than or equal to ninety degrees with respect to a meplat of the projectile.