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.

Patent No.:

US 6964154 B1

PDF
Full Text
Expired
Date of Patent:
Nov. 15, 2005

Filed:

Mar. 11, 2003
Applicants:

Robert L. Sackheim, Madison, AL (US);

John J. Hutt, Decatur, AL (US);

William E. Anderson, West Lafayette, IN (US);

Gordon A. Dressler, Manhattan Beach, CA (US);

Inventors:

Robert L. Sackheim, Madison, AL (US);

John J. Hutt, Decatur, AL (US);

William E. Anderson, West Lafayette, IN (US);

Gordon A. Dressler, Manhattan Beach, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F02K003/00 ; F02K007/00 ; F02K009/00 ; F02K009/74 ; F02K009/76 ;
U.S. Cl.
CPC ...
Abstract

A rocket engine assembly is provided for a vertically launched rocket vehicle. A rocket engine housing of the assembly includes two or more combustion chambers each including an outlet end defining a sonic throat area. A propellant supply for the combustion chambers includes a throttling injector, associated with each of the combustion chambers and located opposite to sonic throat area, which injects the propellant into the associated combustion chamber. A modulator, which may form part of the injector, and which is controlled by a controller, modulates the flow rate of the propellant to the combustion chambers so that the chambers provide a vectorable net thrust. An expansion nozzle or body located downstream of the throat area provides expansion of the combustion gases produced by the combustion chambers so as to increase the net thrust.


Find Patent Forward Citations

Sackheim, Robert. (2005). Axisymmetric, throttleable non-gimballed rocket engine (U.S. Patent No. 6964154). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/6964154

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

Loading…