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:
Jul. 28, 2009

Filed:

Feb. 25, 2005
Applicants:

Donald Gerrit Nyberg, Redmond, WA (US);

Thomas Adrian Groudle, Redmond, WA (US);

Richard Doyle Smith, Kirkland, WA (US);

Inventors:

Donald Gerrit Nyberg, Redmond, WA (US);

Thomas Adrian Groudle, Redmond, WA (US);

Richard Doyle Smith, Kirkland, WA (US);

Assignee:

GHKN Engineering LLC, Redmond, WA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

The thrust of a rocket motor can be varied while maintaining efficiency over a range of pressure ratios using a design that allows for changing the relative position of a plug and a combustion chamber exit. The plug or the chamber exit may be attached to an adaptive control system for position modification. The plug may be positioned in a plug nozzle configuration or in an expansion-deflection (ED) configuration. In either configuration, the elongated downstream portion of the plug allows for efficiency over a wide range of pressure ratios, while ability to change plug position with respect to the chamber exit allows adjustment of rocket thrust.


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