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:
Jan. 23, 2024

Filed:

Feb. 24, 2021
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Joseph A. Carmody, Tucson, AZ (US);

Benjamin C. Hulbert, Tucson, AZ (US);

Ryan J. Paffenroth, Tucson, AZ (US);

Andrew J. Harris, Tucson, AZ (US);

Assignee:

Raytheon Company, Tewksbury, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/32 (2006.01); F02K 9/26 (2006.01); F42B 15/10 (2006.01); F42B 5/10 (2006.01); F42B 15/00 (2006.01); F02K 9/97 (2006.01); F42B 14/00 (2006.01);
U.S. Cl.
CPC ...
F02K 9/32 (2013.01); F02K 9/26 (2013.01); F02K 9/978 (2013.01); F42B 5/10 (2013.01); F42B 5/105 (2013.01); F42B 14/00 (2013.01); F42B 15/00 (2013.01); F42B 15/10 (2013.01);
Abstract

A rocket motor for a gun-fired projectile is configured stiffen the burnable propellant in the rocket motor during burning and/or protect the rocket motor from the pressure that occurs during firing of the projectile from the gun. The rocket motor may include a rigid structure that is integrated into the burnable propellant grain to stabilize the burnable propellant grain during burning of the burnable propellant grain. The rigid structure has a matrix or truss-like shape that extends into the depth of the burnable propellant grain. The rocket motor may include a baffled end cap that covers a nozzle of the rocket motor. The end cap defines a baffled path through the end cap to dampen gas flow into the nozzle and prevent particles of the gun propellant from entering the rocket motor. A rocket motor may implement the rigid structure or the baffled end cap, or both structures.


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