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:
Oct. 10, 2017

Filed:

Mar. 03, 2003
Applicants:

Kenneth J. Graham, Warrenton, VA (US);

Edna M. Grove, Chester Gap, VA (US);

Robert D. Lynch, Warrenton, VA (US);

Guy B. Spear, Orlean, VA (US);

Inventors:

Kenneth J. Graham, Warrenton, VA (US);

Edna M. Grove, Chester Gap, VA (US);

Robert D. Lynch, Warrenton, VA (US);

Guy B. Spear, Orlean, VA (US);

Assignee:

AEROJET-GENERAL CORPORATION, Rancho Cordova, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/28 (2006.01); F02K 9/12 (2006.01); F02K 9/95 (2006.01); C06B 45/10 (2006.01); C06B 45/12 (2006.01); C06B 25/34 (2006.01); C06B 29/22 (2006.01); F42B 15/00 (2006.01); F42C 15/36 (2006.01); C06B 45/34 (2006.01);
U.S. Cl.
CPC ...
F42B 15/00 (2013.01); C06B 29/22 (2013.01); C06B 45/10 (2013.01); C06B 45/12 (2013.01); C06B 45/34 (2013.01); F02K 9/12 (2013.01); F02K 9/28 (2013.01); F02K 9/95 (2013.01); F42C 15/36 (2013.01);
Abstract

Solid propellant systems include a main propellant and a secondary propellant in contact with the first propellant that exhibits autoignition temperatures of at least about 100° F. lower than the autoignition temperature of the main propellant. The secondary propellant of the present invention is most advantageously employed with conventional AP-containing solid propellant formulations as the main propellant, especially formulations containing both AP, an energetic solid, and a binder. In especially preferred forms, the secondary propellant will include a nitramine which is at least one selected from nitroguanidine (NQ), cyclotrimethylene trinitramine (RDX) and cyclotetramethylenetetranitramine (HMX), and a binder which is at least one selected from HTPB, HTPE or glycidyl azide polymer (GAP). Most preferably, the secondary propellant will include a combination of nitramines which includes NQ and one of RDX or HMX.


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