US12669317 - Counterweight projectile

The invention describes a counterweight projectile composed of two hemispherical shells that encase a spherical spring and a content, designed to enhance stability and accuracy during flight. Upon impact, the spring compresses and triggers an explosion of the shells, dispersing the contained material effectively.
Claim 1
1 . A counterweight projectile having an upper hemispherical shell and a lower hemispherical shell combined to form a sphere, each of the upper and lower hemispherical shells having a plurality of grooves on an inner surface thereof, wherein a hollow space is formed between the upper and lower hemispherical shells to contain a content, wherein the counterweight projectile comprises a spherical spring accommodated in the hollow space of the upper and lower hemispherical shells, wherein the spherical spring is in a shape of a plurality of coils wound along the inner surfaces of the upper and lower hemispherical shells, and is completely supported and held on the inner surfaces of the upper and lower hemispherical shells, wherein after being launched, the counterweight projectile is configured to shoot forward, stably, straight and evenly to an impact point, and after contacting the impact point, the spherical spring is squeezed and configured to be restored to explode the upper and lower hemispherical shells thereby spreading the content.
Google Patents
https://patents.google.com/patent/US12669317
USPTO PDF
https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/12669317