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:
Dec. 07, 2021

Filed:

Jul. 13, 2017
Applicant:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Inventors:

Robert S. Larson, Harrisville, UT (US);

Royce Beal, Bear River City, UT (US);

Assignee:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C06B 23/00 (2006.01); C06B 29/22 (2006.01); F02K 9/08 (2006.01); B64G 1/40 (2006.01); F02K 9/26 (2006.01);
U.S. Cl.
CPC ...
C06B 23/007 (2013.01); B64G 1/403 (2013.01); C06B 29/22 (2013.01); F02K 9/08 (2013.01); F02K 9/26 (2013.01); F05D 2220/80 (2013.01);
Abstract

A precursor formulation comprising, before curing, a hydroxyl-terminated polybutadiene (HTPB) prepolymer or a hydroxyl-terminated polyether (HTPE) prepolymer, an oxidizer, a dimer fatty diol, and an isocyanate curative. A solid propellant comprising a reaction product of the HTPB prepolymer or HTPE prepolymer, the dimer fatty diol, and the isocyanate curative is also disclosed, as is a rocket motor comprising a case and a solid propellant in the case, the solid propellant comprising the reaction product and an oxidizer. A method of reducing a burn rate of a solid propellant is also disclosed.


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