Method and apparatus for a projectile incorporating a metastable interstitial composite material

• US 8,001,879 B2
• Filed: 01/05/2011
• Issued: 08/23/2011
• Est. Priority Date: 06/03/2005
• Status: Expired due to Fees

• Current Assignee: NEWTEC Services Group, Inc.
• Original Assignee: NEWTEC Services Group, Inc.
• Inventors: Maston, Michael Joseph, Williams, Keith
• Primary Examiner(s): Chambers; Troy
• Application Number:
  US12/984,894
• Publication Number:
  US 20110100245A1
• Time in Patent Office: 230 Days
• Field of Search: 102/302, 102514-528, 86/54
• US Class Current: 86/54
• CPC Class Codes: F42B 12/22 with fragmentation-hull construction
• CPC Class Codes: F42B 12/56 for dispensing discrete solid bodies F42B12/70 takes precedence
• CPC Class Codes: F42B 12/74 of the core or solid body

Abstract

A method and apparatus for incorporating nanophase elemental materials and metastable interstitial composite materials into projectiles, projectile fragments, ordnance casings, warheads and structural components. The projectile, fragments and casings include an elemental material capable of oxidizing. A coating material that is capable of preventing oxidation of the elemental material and an oxidizing agent may be present and be capable of reacting with the elemental material so that a self-propagating high temperature synthesis reaction from a stabilized solid material is yielded for the purpose of rendering terminal effects or thermal impact to a target at impact.

Claims

1. A method of manufacturing a projectile that can create a thermal event comprising swaging an oxidizing agent with an elemental material into a desired shape, wherein the elemental material has a purity of at least approximately 75% and at least 90% of the elemental material oxidizes within approximately 10 seconds of exposure to oxygen to produce the thermal event.

2. The method as in claim 1 further comprising coating the elemental material with at least one of polytetrafluoroethylene, perfluoroalkoxy, fluorinated ethylene propylene, polyamide, PVC vinyl, steric acid, or carbonyl acid.

3. The method as in claim 1, further comprising coating the elemental material with a coating material to prevent oxidation of the elemental material.

4. The method as in claim 3, further comprising removing the coating material from the elemental material.

5. The method as in claim 3 further comprising swaging the oxidizing agent, elemental material, and coating material into the desired shape.

6. The method as in claim 1, further comprising surrounding the desired shape with a full metal jacket.

7. The method as in claim 1, further comprising swaging a ballast material with the elemental material.

8. The method as in claim 1, further comprising swaging the elemental material into a plurality of desired shapes and joining the plurality of desired shapes to form the projectile.

9. The method as in claim 8, further comprising encasing the plurality of desired shapes in a casing.

10. A method of manufacturing a projectile that can create a thermal event comprising swaging a coated elemental material into a desired shape, wherein the coated elemental material has a purity of at least approximately 75% and at least approximately 90% of the elemental material oxidizes within approximately 10 seconds of exposure to oxygen to produce the thermal event.

11. The method as in claim 10, further comprising swaging an oxidizing agent with the coated elemental material into the desired shape.

12. The method as in claim 10, further comprising surrounding the desired shape with a full metal jacket.

13. The method as in claim 10, further comprising swaging a ballast material with the elemental material.

14. The method as in claim 10, further comprising swaging the elemental material into a plurality of desired shapes and joining the plurality of desired shapes to form the projectile.

15. The method as in claim 14, further comprising encasing the plurality of desired shapes in a casing.

16. The method as in claim 10, further comprising attaching an explosive charge to the desired shape.

17. The method as in claim 16, further comprising attaching a detonator to the explosive charge.