The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 14, 2012

Filed:

Mar. 27, 2009
Applicants:

Eric L. Petersen, College Station, TX (US);

Sudipta Seal, Orlando, FL (US);

Matthew Stephens, Elkton, MD (US);

David L. Reid, Orlando, FL (US);

Rodolphe Carro, Melbourne, FL (US);

Thomas Sammet, Orlando, FL (US);

Alex Lepage, Oviedo, FL (US);

Inventors:

Eric L. Petersen, College Station, TX (US);

Sudipta Seal, Orlando, FL (US);

Matthew Stephens, Elkton, MD (US);

David L. Reid, Orlando, FL (US);

Rodolphe Carro, Melbourne, FL (US);

Thomas Sammet, Orlando, FL (US);

Alex Lepage, Oviedo, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C06B 45/00 (2006.01); C06B 45/18 (2006.01); C06B 29/00 (2006.01); C06B 29/02 (2006.01); D03D 23/00 (2006.01); D03D 43/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

Solid composite propellant compositions include at least one oxidizing agent, at least one binder, and at least one surfactant. The surfactant provides the solid propellant the property of being 'self-extinguishing', where the burning rate of the solid composite propellant as a function of pressure includes a negative pressure dependence portion, wherein the burning rate in the negative pressure dependence portion decreases with increasing pressure until a cutoff pressure is reached which results in extinguishment of the solid composite propellant. The solid composite propellant can also include at least one catalyst that modifies the burning rate of the solid composite propellant. Solid composite propellants can be extinguished without the need for depressurization by reaching a cutoff pressure, and with a tailored burning rate.


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