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. 27, 2024

Filed:

May. 20, 2021
Applicant:

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

Inventors:

Chelsey Hargather, Socorro, NM (US);

Mark Kaufman, Auburn, CA (US);

Michael McPherson, Socorro, NM (US);

Jillian Marsh, Austin, TX (US);

Matthew Hinton, Socorro, NM (US);

Dane Fradenburg, Socorro, NM (US);

Maureen Gannon, San Francisco, CA (US);

Jason Hundley, Albuquerque, NM (US);

Michael Hargather, Socorro, NM (US);

Assignee:

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

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/24 (2006.01); B29C 64/314 (2017.01); B33Y 70/10 (2020.01); F02K 9/10 (2006.01); B29C 64/386 (2017.01); B29C 64/371 (2017.01); B33Y 40/00 (2020.01); B33Y 50/00 (2015.01); F02K 9/72 (2006.01); F02K 9/18 (2006.01); B29L 31/20 (2006.01); B29K 55/02 (2006.01);
U.S. Cl.
CPC ...
F02K 9/24 (2013.01); B29C 64/314 (2017.08); B29C 64/371 (2017.08); B29C 64/386 (2017.08); B33Y 40/00 (2014.12); B33Y 50/00 (2014.12); B33Y 70/10 (2020.01); F02K 9/10 (2013.01); F02K 9/18 (2013.01); F02K 9/72 (2013.01); B29K 2055/02 (2013.01); B29L 2031/20 (2013.01);
Abstract

A method of making a fuel grain for use in a rocket motor, the method comprising blending a first energetic nanoscale metallic compound and a second compound suitable to form a feedstock material for use in an additive manufacturing apparatus, the additive manufacturing apparatus operatively connected to a computing system, that provides additive manufacturing printing instructions to the additive manufacturing apparatus, permitting construction of an autonomously designed and optimized rocket fuel grain section; wherein the stochastic deposition simulation-assisted fuel grain geometries further comprise a plurality of agglutinated layers of solidified fuel grain compound, each layer of the plurality of layers comprising a plurality of blended and radially displaced beads of different radii, said radial displacement optionally optimized via competitive simulation programs, and wherein the system continuously mixes constituent materials in an inline/static mixer, with viscosity controlled via particle size variations, and material is deposited in a controlled atmosphere or vacuum.


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