High kinetic energy hollow bullet

A bullet which comprises:

• a brass casing containing smokeless gun powder;
• a plastic wad disposed within the brass casing and positioned adjacent to the smokeless gun powder;
• and
• a nozzled projectile operatively coupled to the plastic wad, and wherein:
• iii. the nozzled projectile is hollow and includes an internal tapered structure made of a metal alloy, extending longitudinally from a proximal end to a distal end, with the diameter at the proximal end being at least twice a diameter at the distal end;
• ii. the internal tapered structure is configured to create a venturi effect during flight of the bullet to enhance kinetic energy and stability;
• iii. the nozzled projectile further includes an exterior aerodynamically optimized shape and an external ballistic tip at the distal end for maximized penetration upon impact, and wherein the nozzled projectile has a point located adjacent to the proximal end which is wider in diameter than the proximal end, and wherein the nozzled projectile widens in diameter and is conically shaped from the point adjacent the proximal end to the distal end.

A method of operating a hollow bullet comprising the steps of:

• a. loading a bullet into a firearm, wherein the bullet includes a brass casing containing smokeless gun powder, a plastic wad, and a nozzled projectile with an internal tapered structure made of a metal alloy;
• b. firing the bullet from the firearm, wherein the ignition of the smokeless gun powder by a firing mechanism causes a rapid expansion of gases within the brass casing;
• c. propelling the nozzled projectile through the barrel of the firearm, wherein the plastic wad seals the gases and directs them towards the nozzled projectile;
• d. allowing air to enter the hollow nozzled projectile at a proximal end and pass through the internal tapered structure, creating a venturi effect that enhances the kinetic energy and stability of the bullet during flight;
• e. maintaining the bullet's trajectory and stability through an aerodynamically optimized shape of the nozzled projectile;
• and
• f. achieving maximized penetration upon impact with the target, facilitated by the external ballistic tip at a distal end of the nozzled projectile, and wherein the nozzled projectile has a point located adjacent to the proximal end which is wider in diameter than the proximal end, and wherein the nozzled projectile widens in diameter and is conically shaped from the point adjacent the proximal end to the distal end.