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:
Feb. 09, 2021

Filed:

Feb. 14, 2018
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Neil Evan Goodzeit, Woodside, CA (US);

John B. Henderson, Littleton, CO (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); B64G 1/26 (2006.01); B64G 1/00 (2006.01);
U.S. Cl.
CPC ...
B64G 1/401 (2013.01); B64G 1/007 (2013.01); B64G 1/26 (2013.01); B64G 1/402 (2013.01);
Abstract

Systems and methods of the present disclosure can be utilized to provide an improved propulsion system that uses multiple high efficiency engines to provide fault-tolerant and scalable high thrust for orbit transfer and maneuvering over life. An exemplary spacecraft includes a base panel, a cylindrical core member mounted to the base panel, multiple DV thrusters mounted within the cylindrical core member, and multiple reaction engine assemblies mounted to the base panel outside the cylindrical core member. Each of the DV thrusters has a thrust level that is greater than a thrust level of each of the reaction engine assemblies. The multiple DV thrusters are operated for velocity control, with attitude control being performed by off-pulsing at least one of the multiple DV thrusters.


Find Patent Forward Citations

Goodzeit, Neil. (2021). Fault-tolerant scalable high thrust spacecraft propulsion (U.S. Patent No. 10913551). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10913551

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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