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:
Aug. 20, 2024

Filed:

Nov. 03, 2023
Applicant:

Government of the United States As Represented BY the Secretary of the Air Force, Rome, NY (US);

Inventor:

Jonathan Allison, Albuquerque, NM (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); F02K 9/42 (2006.01); F02K 9/44 (2006.01); F02K 9/48 (2006.01); F02K 9/50 (2006.01); F02K 9/56 (2006.01); F02K 9/58 (2006.01);
U.S. Cl.
CPC ...
B64G 1/4021 (2023.08); B64G 1/401 (2013.01); B64G 1/402 (2013.01); B64G 1/4024 (2023.08); F02K 9/42 (2013.01); F02K 9/44 (2013.01); F02K 9/48 (2013.01); F02K 9/50 (2013.01); F02K 9/56 (2013.01); F02K 9/566 (2013.01); F02K 9/58 (2013.01);
Abstract

A system for managing propellant and pressurant for in-space propulsion of a spacecraft is provided. The system includes a conformal fuel tank having an ullage operatively connected for pressurization and a propellant management device (PMD) to wick propellant to a liquid port of the conformal fuel tank. The system further includes a pneumatic circuit including a tank pressurant vent valve for adjustment of operating pressure prior to refueling operations; a vent to release excess pressurant; a pressurant metering vent valve to provide control and safety relief for the pressurant; a check valve to prevent backflow; a pressurant cat bed for decomposing propellant into pressurant; a repressurizing valve to release pressurant once cooled; a burst disk to provide overpressure safety relief; a series of propellant extraction valves to intake a predetermined quantity of propellant for decomposition; and a pressure regulator that delivers proper pressure to a series of thrusters.


Find Patent Forward Citations

Allison, Jonathan. (2024). System and method for asynchronous autogenously pressurized in-space propulsion (U.S. Patent No. 12065270). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12065270

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

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