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:
May. 09, 2023

Filed:

Dec. 23, 2020
Applicant:

Radian Aerospace, Inc., Renton, WA (US);

Inventors:

Livingston L. Holder, Renton, WA (US);

Gary C. Hudson, Renton, WA (US);

Bevin C. McKinney, Renton, WA (US);

Assignee:

Radian Aerospace, Inc., Renton, WA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/52 (2006.01); B64G 1/14 (2006.01); B64G 1/40 (2006.01); F02K 9/42 (2006.01); F02K 9/56 (2006.01); F02K 9/60 (2006.01); F02K 9/82 (2006.01); F02K 9/86 (2006.01);
U.S. Cl.
CPC ...
F02K 9/52 (2013.01); B64G 1/14 (2013.01); B64G 1/401 (2013.01); F02K 9/42 (2013.01); F02K 9/566 (2013.01); F02K 9/605 (2013.01); F02K 9/82 (2013.01); F02K 9/86 (2013.01);
Abstract

Rocket propulsion systems and associated methods are disclosed. A representative system includes a combustion chamber having an inwardly-facing chamber wall enclosing a combustion zone. The chamber has a generally spherical shape and is exposed to the combustion zone. A propellant injector is coupled to the combustion chamber and has at least one fuel injector nozzle positioned to direct a flow of cooling fuel radially outwardly along the inwardly-facing chamber wall. In addition to or in lieu of the foregoing features, the injector can include an oxidizer piston and a fuel piston that deliver oxidizer and fuel, respectively, to the combustion chamber, in a sequenced manner so that the oxidizer is introduced prior to the fuel.


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