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. 01, 2020

Filed:

Dec. 01, 2017
Applicant:

Northrop Grumman Innovation Systems, Inc., Plymouth, MN (US);

Inventors:

Christine A. Agathon-Burton, Bethesda, MD (US);

Matthew Alan Michel, Oak Hill, VA (US);

Dewey Edwin Cochran, Arlington, VA (US);

Ronald Lynn Graham, Herndon, VA (US);

Gregg A. Herbert, Waterford, VA (US);

William A. Llorens, Herndon, VA (US);

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/52 (2006.01); B64G 1/64 (2006.01); B64G 1/40 (2006.01); B64G 1/10 (2006.01);
U.S. Cl.
CPC ...
B64G 1/52 (2013.01); B64G 1/405 (2013.01); B64G 1/646 (2013.01); B64G 1/1078 (2013.01);
Abstract

Methods and systems for mitigating or reducing the risk of an electrostatic discharge due to static charge differentials between a first spacecraft and a second spacecraft as the first spacecraft approaches the second spacecraft may be accomplished using a passive electrostatic discharge mitigation device. In some embodiments, mitigation of static potential between the first spacecraft and the second spacecraft may be actively accomplished by an electric propulsion system provided on the first spacecraft. In some embodiments, mitigation may be provided by both actively and passively mitigating static potential between the first spacecraft and the second spacecraft.


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