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. 13, 2022

Filed:

Jan. 31, 2021
Applicant:

Momentus Space Llc, San Jose, CA (US);

Inventors:

Jason Hummelt, San Jose, CA (US);

Joel Sercel, Lake View Terrace, CA (US);

Philip Mainwaring, San Jose, CA (US);

James Small, Sonoita, AZ (US);

Matthew Parman, Mountain View, CA (US);

Assignee:

MOMENTUS SPACE LLC, San Jose, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); H01J 37/32 (2006.01); F03H 1/00 (2006.01);
U.S. Cl.
CPC ...
H01J 37/32247 (2013.01); B64G 1/405 (2013.01); B64G 1/409 (2013.01); F03H 1/0093 (2013.01);
Abstract

A multi-mode thruster system for use in a spacecraft includes a microwave source; a cavity coupled to the microwave source and including a first inlet to receive a first fluid and a second inlet to receive a second fluid; and a nozzle provided at one end of the cavity. The thruster operates in a microwave electrothermal thruster (MET) mode to (i) generate a standing wave in the cavity using the microwave source and (ii) raise a temperature of the first fluid to generate a first hot gas that exits the cavity via the nozzle to generate thrust. The thruster operates in a chemical propulsion mode to (i) produce a reduction-oxidation reaction between the first fluid and the second fluid and (ii) generate a second hot gas that exits the cavity via the nozzle to generate thrust.


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