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. 09, 2022

Filed:

Aug. 11, 2020
Applicants:

Stephen Whitmore, Logan, UT (US);

Mark C. Heiner, Logan, UT (US);

Inventors:

Stephen Whitmore, Logan, UT (US);

Mark C. Heiner, Logan, UT (US);

Assignee:

Utah State University, Logan, UT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/72 (2006.01); F02K 9/26 (2006.01); F02K 9/52 (2006.01); F02K 9/14 (2006.01);
U.S. Cl.
CPC ...
F02K 9/72 (2013.01); F02K 9/14 (2013.01); F02K 9/26 (2013.01); F02K 9/52 (2013.01);
Abstract

A hybrid rocket includes a housing having first and second ends, a solid-grain fuel material in the housing and defining a bore extending from end to end, two electrodes positioned adjacent to the fuel material to ignite the fuel material at the first end, a primary oxidizer port positioned at the first end to inject a primary oxidizer to flow in a downstream direction from the first end to the second end, a nozzle positioned at the second end and having a converging portion and a diverging portion, and a secondary oxidizer port to inject a secondary oxidizer downstream of the converging portion. The bore has a geometry configured to produce a hot-gas, fuel-rich mixture at the nozzle as the fuel material and primary oxidizer burn while flowing downstream. The diverging portion of the nozzle is configured to spontaneously combust the secondary oxidizer and the hot-gas, fuel-rich mixture.


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