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:
Jun. 18, 2024

Filed:

May. 09, 2022
Applicant:

Ball Aerospace & Technologies Corp., Boulder, CO (US);

Inventors:

Gordon C. Wu, Lafayette, CO (US);

Derek Chan, Boulder, CO (US);

Robert J. Baltrum, Jr., Longmont, CO (US);

Eric R. Turner, Longmont, CO (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); F02K 9/58 (2006.01); F02K 9/46 (2006.01); F02K 9/44 (2006.01); F02K 9/56 (2006.01); F02K 9/42 (2006.01); F02K 9/50 (2006.01); B64G 1/64 (2006.01);
U.S. Cl.
CPC ...
B64G 1/402 (2013.01); B64G 1/64 (2013.01); F02K 9/42 (2013.01); F02K 9/44 (2013.01); F02K 9/46 (2013.01); F02K 9/50 (2013.01); F02K 9/56 (2013.01); F02K 9/566 (2013.01); F02K 9/58 (2013.01);
Abstract

Chemical propellant storage and supply systems and methods for use on spacecraft are provided. The systems and methods include a fluid pump for moving chemical propellant within the system at selected pressures. This can include operating the fluid pump to supply propellant to a thruster system at a selected pressure. A fuel tank can be refilled by connecting a propellant resupply source to the system, and operating the fluid pump to move propellant from the propellant resupply source to the fuel tank. In a system with multiple fuel tanks, the fluid pump can be operated to move propellant from a donor fuel tank to a recipient fuel tank. The chemical propellant can be stored in one or more fuel tanks at a relatively low pressure. In addition, the chemical propellant is not pressurized by a gaseous pressurant while it is stored in the fuel tank.


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