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. 10, 2017

Filed:

Sep. 23, 2014
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Andrew B. Facciano, Tucson, AZ (US);

Rodney H. Krebs, Oro Valley, AZ (US);

Michael S. Bielas, Tucson, AZ (US);

Cody D. Tretschok, Tucson, AZ (US);

Michael S. Spangler, Vail, AZ (US);

Benjamin Mitchell, Oro Valley, AZ (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F42B 30/00 (2006.01); H01Q 1/42 (2006.01); H01Q 3/24 (2006.01); H01Q 1/28 (2006.01); F42B 15/01 (2006.01); F41G 7/00 (2006.01); F41G 7/22 (2006.01);
U.S. Cl.
CPC ...
F42B 30/006 (2013.01); F41G 7/008 (2013.01); F41G 7/2246 (2013.01); F41G 7/2253 (2013.01); F41G 7/2286 (2013.01); F41G 7/2293 (2013.01); F42B 15/01 (2013.01); H01Q 1/28 (2013.01); H01Q 1/42 (2013.01); H01Q 3/24 (2013.01);
Abstract

An adaptive electronically steerable array (AESA) system comprises a plurality of arrays, each comprising a plurality of radiating elements, each array configured for placement on a forward-facing surface of a different one of a plurality of aerodynamic control surfaces on an interceptor. A plurality of radio frequency (RF) transmissive radome elements, each having an aerodynamic shape complementary to the aerodynamic control surface, are placed over one of the arrays. Control circuitry configures the arrays, independently or in concert, for RF target engagement and communication. Additional arrays may be positioned on side or aft-facing surfaces of the aerodynamic control surfaces for RF communication. The AESA system may be paired with an IR system for dual-mode operation.


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