Propellant compositions containing a staple metal fuel

• US 3,933,543 A
• Filed: 01/15/1964
• Issued: 01/20/1976
• Est. Priority Date: 01/15/1964
• Status: Expired due to Term

• Current Assignee: Atlantic Research Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Atlantic Research Corporation (L3Harris Technologies, Inc.)
• Inventors: Madden, Dale A.
• Primary Examiner(s): Padgett, Benjamin R.
• Assistant Examiner(s): Nelson, P. A.
• Application Number:
  US04/337,955
• Time in Patent Office: 4,388 Days
• Field of Search: 102/98, 102/103, 149/2, 149/19, 149/44, 149/21, 149/37, 149/42, 149/96, 149/114
• US Class Current: 149/21
• CPC Class Codes: C06B 45/00 Compositions or products which are defined by structure or arrangement of component of product explosive charges of particular form or shape F42B1/00, F42B3/00
• CPC Class Codes: Y10S 149/114 Inorganic fuel

Abstract

A gas-generating composition comprising an oxidizer, a non-metal, preferably organic, fuel component, and a metal fuel staple component of a particular size.

Claims

1. In a propellant composition comprising an oxidizing component selected from the group consisting of inorganic perchlorates or nitrates, metal peroxides, hydrazine nitroformate, and mixtures thereof, a non-metal fuel component selected from the group consisting of inert fuels and fuels rendered active by molecularly combined nitroso, nitro, nitrite or nitrate groups, and mixtures thereof and a metal fuel component, the improvement in which the metal is selected from the group consisting of aluminum, beryllium, zirconium, magnesium, titanium, tungsten, alloys thereof, and mixtures thereof, and is in the form of staple having a maximum thickness of about 0.001 inch, a maximum ratio of thickness to width of about 1 to 4, a minimum length of about 0.03 inch and a maximum ratio of width to length of about 1 to 1.

2. The composition of claim 1 in which the metal staple is aluminum.

3. The composition of claim 2 which additionally contains a minor amount by weight, of the total composition, of metal staple selected from the group consisting of silver and copper.

4. The composition of claim 1 in which the propellant composition contains, in addition to said staple, a metal fuel component in the form of a finely divided powder.

5. The composition of claim 4 in which the metal staple is aluminum.

6. The composition of claim 5 which additionally contains a minor amount by weight, of the total composition, of metal staple selected from the group consisting of silver and copper.

7. The composition of claim 1 in which the non-metal fuel component is an organic compound.

8. The composition of claim 7 in which the organic compound is a polymer.

9. The composition of claim 8 in which the oxidizing component is a solid, insoluble, finely divided inorganic oxidizer.

10. The composition of claim 9 in which the metal staple is aluminum.

11. The composition of claim 10 which additionally contains a minor amount by weight, of the total composition, of metal staple selected from the group consisting of silver and copper.

12. The composition of claim 9 in which the oxidizer is ammonium perchlorate.

13. The composition of claim 12 in which the metal staple is aluminum.

16. The composition of claim 2 which additionally contains, in a minor amount by weight of the total composition, metal staple selected from the group consisting of silver and copper.

14. In a gas-generating composition comprising an oxidizing component selected from the group consisting of inorganic perchlorates or nitrates, metal peroxides, hydrazine nitroformate, and mixtures thereof, a non-metal fuel component selected from the group consisting of inert fuels and fuels rendered active by molecularly combined nitroso, nitro, nitrite or nitrate groups, and mixtures thereof, and a metal fuel component, the improvement in which the metal is selected from the group consisting of aluminum, beryllium, zirconium, magnesium, titanium, tungsten, alloys thereof, and mixtures thereof, and is in the form of staple having a maximum thickness of about 0.001 inch, a maximum ratio of thickness to width of about 1 to 4, a minimum length of about 0.03 inch and a maximum ratio of width to length of about 1 to 1.

15. The composition of claim 14 in which the metal staple is aluminum.

17. The composition of claim 14 in which the composition contains, in addition to said staple, a metal fuel component in the form of a finely divided powder.

18. The composition of claim 14 in which the non-metal fuel component is an organic compound.

19. The composition of claim 18 wherein said organic compound is a polymer.

20. The composition of claim 19 in which the oxidizing component is a solid, insoluble, finely divided inorganic oxidizer.