Claims
- 1. A non-lead hollow point bullet comprising:
a mixed construction slug further comprising,
a monolithic metal insert having a hollow point tip and a tail protrusion, an unsintered powdered metal composite core in tandem alignment with said insert, said core having a hollow cavity tip portion coupled with said tail protrusion, a jacket having an open tip and enveloping at least a portion of said insert and said core, said jacket swaged at said open tip.
- 2. A bullet according to claim 1 wherein said insert is selected from the group consisting of tin and polymers.
- 3. A bullet according to claim 1 wherein said unsintered powdered metal composite core is selected from the group consisting of tungsten and tin.
- 4. A bullet according to claim 1 wherein said jacket is a copper alloy.
- 5. A bullet according to claim 1 wherein said insert consists essentially of 40 grain monolithic tin, said core consists essentially of 80 grain tungsten-tin composite with 75 wt % tungsten and 25 wt % tin, and said jacket consists essentially of 20 grain copper alloy.
- 6. A bullet according to claim 1 wherein said hollow point tip, tail protrusion, and hollow cavity tip portion is essentially tapered.
- 7. A bullet according to claim 1 wherein said hollow point tip, tail protrusion, and hollow cavity tip portion is essentially conical.
- 8. A method of forming a non-lead hollow point bullet comprising;
a) compressing an unsintered metal powdered composite core into a jacket, b) punching a hollow cavity tip portion into said core, c) seating an insert, said insert having a hollow point tip and a tail protrusion, on top of said core such that said tail protrusion couples with said hollow cavity tip portion, d) swaging the open tip of said jacket.
- 9. The method according to claim 8 wherein said insert is selected from the group consisting of tin and polymers.
- 10. The method according to claim 8 wherein said unsintered powdered metal composite core is selected from the group consisting of tungsten and tin.
- 11. The method according to claim 8 wherein said jacket is a copper alloy.
- 12. A method according to claim 8 wherein said insert consists essentially of 40 grain monolithic tin, said core consists essentially of 80 grain tungsten-tin composite with 75% by weight tungsten and 25% by weight tin, and said jacket consists essentially of 20 grain copper alloy.
- 13. The method according to claim 8 wherein said swaged jacket tip shape is selected from the group consisting of round nose and truncated cone.
- 14. The method according to claim 8 wherein said compressing step is performed at room temperature and 50,000-psig pressure.
- 15. The method according to claim 8 wherein said hollow point tip, tail protrusion, and hollow cavity tip portion is essentially tapered.
- 16. The method according to claim 8 wherein said hollow point tip, tail protrusion, and hollow cavity tip portion is essentially conical.
STATEMENT REGARDING FEDERAL SPONSORSHIP
[0001] This invention was made with Government support under contract no. DE-AC05-00OR22725 to UT-Battelle, LLC, awarded by the United States Department of Energy. The Government has certain rights in the invention.