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:
Jan. 02, 2024

Filed:

Jul. 29, 2020
Applicant:

Triad National Security, Llc, Los Alamos, NM (US);

Inventors:

Nicholas Dallmann, Los Alamos, NM (US);

Ian Shelburne, Los Alamos, NM (US);

Kavitha Chintam, Los Alamos, NM (US);

Malakai Coblentz, Los Alamos, NM (US);

David Hemsing, Los Alamos, NM (US);

Joseph Lichthardt, Los Alamos, NM (US);

Bryce Tappan, Los Alamos, NM (US);

Mahlon S. Wilson, Los Alamos, NM (US);

Assignee:

TRIAD NATIONAL SECURITY, LLC, Los Alamos, NM (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/86 (2006.01); F02K 9/76 (2006.01); F02K 9/34 (2006.01); F02K 9/28 (2006.01); F02K 9/84 (2006.01);
U.S. Cl.
CPC ...
F02K 9/86 (2013.01); F02K 9/28 (2013.01); F02K 9/34 (2013.01); F02K 9/763 (2013.01); F02K 9/84 (2013.01); F05D 2240/1281 (2013.01);
Abstract

A system for multiple burns from a solid fuel rocket motor may extinguish rocket fuel after the rocket has been ignited. The motor may be extinguished via rapid decompression of the combustion chamber. The fuel may then be reignited by a suitable igniter, and the process of extinguishing and reigniting may be repeated, enabling multi-burn maneuvers. A decompressive extinguishing plug nozzle may extinguish solid rocket fuel after the rocket has been ignited and/or keep a rocket in a disarmed (zero thrust) state until the rocket is to be armed. The nozzle may include a plug that mostly impedes the opening of the nozzle and an outer cowl that is movable to rapidly decompress the combustion chamber. This rapid decompression extinguishes the solid rocket fuel. In some aspects, the fuel can be reignited and extinguished multiple times.


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