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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Trajectory correction kit

Invented by: David A. Bittle
Somerville, AL

Gary T. Jimmerson
Athens, AL

Julian L. Cothran
Arab, AL

Originally Assigned to: The United States of America as represented by the Secretary of the Army
Washington, DC
[Now assigned to . . .]

Issued:2008-08-26
Filed:2005-09-16
Application No:11229425
Examined by:Gregory; Bernarr E

The Trajectory Correction Kit (TCK) is a completely self-contained retrofit kit that is externally and fixedly mounted as an add-on to the rear (aft of the tailfins) of an existing, unguided rocket. The TCK continuously measures the pitch and yaw of the rocket as it is released from the launch tube and during the initial seconds of the flight and calculates the trajectory correction that is necessary to eliminate the measured pitch and yaw. Then it activates selected thrusters among the thrusters that are positioned around the circumference of the rocket body so as to steer the rocket in a direction until the measured pitch and yaw are eliminated. This results in significant reductions in both the rocket flight path dispersion and collateral damage.

[pdf] U.S. Pat. No. 7,416,154

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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