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. 16, 2025

Filed:

Jun. 06, 2023
Applicant:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Inventors:

James Garret Nicholson, Broadlands, VA (US);

Daniel Carl Treachler, Leesburg, VA (US);

Oliver Benjamin Ortiz, Beltsville, MD (US);

James Dulin Reavill, Irving, TX (US);

Benjamin Michael Hekman, Percellville, VA (US);

Robert Bryan Sullivan, Chantilly, VA (US);

Carlos Guillermo Niederstrasser, Reston, VA (US);

Mark Lieberbaum, Arlington, VA (US);

Michael Joseph Glogowski, Leesburg, VA (US);

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

Kenneth Siu-Kin Chow, Great Falls, VA (US);

Peter Michael Cipollo, Arlington, VA (US);

Assignee:

Northrop Grumman Systems Corporation, Falls Church, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/10 (2006.01); B64G 1/24 (2006.01); B64G 1/26 (2006.01); B64G 1/40 (2006.01); B64G 1/64 (2006.01);
U.S. Cl.
CPC ...
B64G 1/1078 (2013.01); B64G 1/2427 (2023.08); B64G 1/26 (2013.01); B64G 1/264 (2023.08); B64G 1/40 (2013.01); B64G 1/402 (2013.01); B64G 1/4024 (2023.08); B64G 1/643 (2023.08); B64G 1/646 (2013.01); B64G 1/6462 (2023.08); B64G 1/6464 (2023.08); B64G 1/2429 (2023.08);
Abstract

Spacecraft servicing devices or pods and related methods may include a body configured to be deployed from a host spacecraft at a location adjacent a target spacecraft and at least one spacecraft servicing component configured to perform at least one servicing operation on the target spacecraft. The spacecraft servicing device may include a thruster assembly coupled to a boom arm, where the boom arm is configured to alter an orientation of the thruster assembly as the boom arm is rotated about the spacecraft body and a docking device.


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