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:
Mar. 17, 2020

Filed:

Apr. 23, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

James P. Scott, Manhattan Beach, CA (US);

Michael A. Whelan, Rancho Palos, CA (US);

Bradley A. Scott, Silverado, CA (US);

Dennis L. Gould, Whittier, CA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H04J 14/02 (2006.01); H04B 10/2575 (2013.01); H04B 10/118 (2013.01); H04B 10/27 (2013.01);
U.S. Cl.
CPC ...
H04J 14/0204 (2013.01); H04B 10/118 (2013.01); H04B 10/25755 (2013.01); H04B 10/271 (2013.01); H04J 14/022 (2013.01); H04J 14/0205 (2013.01);
Abstract

A satellite payload system is disclosed. The satellite payload system includes a plurality of optical processing modules, each including: a module input including an optical splitter, a module output including an optical coupler, a dynamic gain equalizer, an output bank of optical filters, and an input bank of optical filters; where the plurality of optical processing modules include ring-connected optical processing modules and inter-satellite optical processing modules; and at least one optical fiber ring communicatively coupled to each of the ring-connected optical processing modules; where at least one of the ring-connected optical processing modules is configured to provide on-board signal processing of wavelengths; where a plurality of the ring-connected optical processing modules are each communicatively coupled to a respective inter-satellite optical processing module; where each inter-satellite optical processing module is configured to optically communicatively couple to a respective remote satellite via its module input and via its module output.


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