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. 27, 2004

Filed:

Jan. 08, 2002
Applicant:
Inventors:

Mark P. Friedlander, III, Centerville, VA (US);

Michael D. Allen, Manassas, VA (US);

Stephen H. Tse, Jr., Dale City, VA (US);

Roger S. Snyder, Front Royal, VA (US);

Guy B. Spear, Orlean, VA (US);

Assignee:

Atlantic Research Corporation, Gainesville, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/06 ;
U.S. Cl.
CPC ...
F02K 1/06 ;
Abstract

Control apparatus for a nozzle for a rocket or other vehicle having a combustion chamber with a propellant therein in communication with the nozzle, the nozzle having a throat and a pair of bores extending into the throat The bores may be in opposed or any other suitable relation. A pair of plungers are slidably mounted in the bores and are movable between an open position wherein they are disposed outside of the throat and a closed position wherein they extend into the throat to substantially close it. The plungers have a width or diameter substantially the same as the width or diameter of the throat. Actuator devices are provided for moving the plungers independently of each other to control thrust by controlling the flow of combustion gases through the throat and the pressure in the combustion chamber. The movement of the plungers can also be used for thrust vector control.


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