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. 05, 2021

Filed:

Dec. 03, 2019
Applicant:

Us Government As Represented BY Sec'y of Air Force, Wright-Patterson AFB, OH (US);

Inventors:

Geremy Kleiser, Niceville, FL (US);

Christopher Crouse, Valparaiso, FL (US);

Christopher Lindsay, Niceville, FL (US);

Ian Kowalczyk, King of Prussia, PA (US);

Walter McCracken, Safety Harbor, FL (US);

Alan Yeates, Yellow Springs, OH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F42B 12/22 (2006.01); F41G 7/00 (2006.01);
U.S. Cl.
CPC ...
F42B 12/22 (2013.01); F41G 7/00 (2013.01); H01M 2220/20 (2013.01);
Abstract

A munition includes a munition body containing explosive material. An electronic subsystem is active between release and detonation of the explosive material. One or more batteries are electrically connected to the electronic subsystem to provide power to the electronic subsystem prior to detonation. The one or more batteries are positioned adjacent to the explosive material to be accelerated outward as corresponding munition projectiles after detonation, increasing the effective payload of the munition by performing dual functions. In one or more embodiments, the explosive material is cylindrically shaped and longitudinally aligned in a warhead section of the munition body. The one or more batteries are annularly positioned on lateral surface of the explosive surface to form a cellular fragmenting structure. In a particular embodiments, the munition body is a missile body containing a rocket propulsion system and the electronic subsystem comprises a missile guidance system.


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