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. 26, 2023

Filed:

May. 20, 2021
Applicant:

X-bow Launch Systems Inc., Albuquerque, NM (US);

Inventors:

Jason Hundley, Albuquerque, NM (US);

Mark Kaufman, Auburn, CA (US);

Michael McPherson, Socorro, NM (US);

Assignee:

X-Bow Launch Systems Inc., Albuquerque, NM (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/24 (2006.01); F02K 9/10 (2006.01); B33Y 80/00 (2015.01); B33Y 10/00 (2015.01);
U.S. Cl.
CPC ...
F02K 9/24 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F02K 9/10 (2013.01); F05D 2220/80 (2013.01); F05D 2230/30 (2013.01);
Abstract

A method of making a multi-grained fuel grain for a rocket is disclosed, the method comprising the steps of using at least one nozzle to extrude a first propellant in an additive manufacturing process, the first propellant comprising a multi-grained fuel grain, the multi-grained fuel grain forming the at least one void, the at least one void facilitating variation in internal ballistics, forming sensors, said sensors permitting continuous monitoring and continuous modification such that a user controls the ballistics profile of a rocket motor, forming an electrically-controlled second propellant in contact with and operatively coupled to the sensors; and wherein the additive manufacturing process uses at least at least one nozzle to extrude raw materials.


Find Patent Forward Citations

Loading…