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. 10, 2019

Filed:

Jan. 17, 2017
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Jeffery P. Sowers, Sahuarita, AZ (US);

Matthew B. Castor, Tucson, AZ (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F41A 21/46 (2006.01); F41A 21/32 (2006.01); F41F 1/06 (2006.01); F41F 1/08 (2006.01); F41F 3/073 (2006.01); F41B 11/73 (2013.01); F41A 21/16 (2006.01);
U.S. Cl.
CPC ...
F41A 21/46 (2013.01); F41A 21/16 (2013.01); F41A 21/32 (2013.01); F41B 11/73 (2013.01); F41F 1/06 (2013.01); F41F 1/08 (2013.01); F41F 3/073 (2013.01);
Abstract

A launcher for launching a projectile includes a launch piston for engaging and driving the projectile from the launcher and a launch brake that constrains the piston to enable separation of the piston from the projectile. The launch brake is configured to have minimal to no effect on projectile exit velocity and exit trajectory from the launcher. The launch brake is also configured to reduce the velocity of the launch piston via coupling of the masses of the launch piston and the launch brake. The coupling allows, separation of the projectile from the launch piston and reduces or prevents a negative effect on stabilization of the projectile upon exit from the launcher.


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