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:
Sep. 05, 2023

Filed:

Nov. 13, 2020
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Christopher M. Cosner, Manhattan Beach, CA (US);

John F. Stickelmaier, Manhattan Beach, CA (US);

John J. Wootan, Hermosa Beach, CA (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02J 7/00 (2006.01); H02J 7/35 (2006.01); H02S 40/38 (2014.01); B64G 1/42 (2006.01); B64G 1/44 (2006.01); B64G 1/58 (2006.01); H01M 10/42 (2006.01); H02S 50/00 (2014.01);
U.S. Cl.
CPC ...
H02J 7/35 (2013.01); B64G 1/425 (2013.01); B64G 1/428 (2013.01); B64G 1/443 (2013.01); B64G 1/58 (2013.01); H01M 10/425 (2013.01); H02J 7/007 (2013.01); H02J 7/0014 (2013.01); H02J 7/0024 (2013.01); H02J 7/0063 (2013.01); H02S 40/38 (2014.12); H02S 50/00 (2013.01); H01M 2010/4271 (2013.01);
Abstract

An electrical power system has a dual battery configuration that enables sufficient power supply for a spacecraft bus and a payload module being carried by the spacecraft. During a sunlight power mode, power is drawn from a solar array of the bus to power a low-discharge payload of the spacecraft and a high-discharge payload of a payload module. During the sunlight power mode, a low rate discharge battery and a high rate discharge battery are charged by a battery charge management unit of the spacecraft bus. During an eclipse power mode, the low rate discharge battery powers the low-discharge payload of the spacecraft and the high rate discharge battery powers the high-discharge payload of the payload module. The high-rate discharge battery may also be used to power the high-rate discharge payload in the sunlight power mode to meet its high current demands to meet a flexible mission operations.


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