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. 25, 2015

Filed:

Dec. 27, 2013
Applicant:

Raytheon Company, Waltham, MA (US);

Inventors:

Andrew B Facciano, Tucson, AZ (US);

Michael S Alkema, Sahuarita, AZ (US);

Michael A Leal, Tucson, AZ (US);

Daniel Chasman, Tucson, AZ (US);

Robert T Moore, Tucson, AZ (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F42B 10/66 (2006.01); F42B 15/01 (2006.01); F42B 10/00 (2006.01); F42B 10/60 (2006.01);
U.S. Cl.
CPC ...
F42B 15/01 (2013.01); F42B 10/663 (2013.01); F42B 10/60 (2013.01); F42B 10/66 (2013.01);
Abstract

A projectile includes a propulsion booster for producing pressurized gases, a nozzle for expelling the pressurized gases produced by the booster, and a supplementary integrated actuation system. The integrated actuation system selectively directs propellant from a storage reservoir of the integrated actuation system through an interiorly-located outlet of the integrated actuation system located at the nozzle and into the nozzle, thus changing a direction of the pressurized gases expelled by the booster. The integrated actuation system also selectively directs propellant from the storage reservoir through a peripherally-located outlet of the integrated actuation system, to produce thrust at an external periphery of the projectile, thus diverting the projectile. The integrated actuation system may also selectively direct propellant to a nozzle actuation system for positioning the nozzle, to a stage separation system for separating portions of the projectile, or to a power generator for generating electric power for the projectile.


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