A system for deploying a plurality of independent payloads with a launch vehicle, the launch vehicle being longitudinally oriented about an axis, includes a plurality of launch modules. Each respective launch module of the plurality of launch modules includes a plurality of package elements. A respective predetermined set of package elements of the plurality of package elements comprises a respective payload of the plurality of payloads. Each respective launch module of the plurality of launch modules is situated in an abuttingly supporting relation with at least one adjacent launch module in a facing relation at an interface in a launch orientation. The interface is generally parallel with the axis. At least one restraining member cooperates with the plurality of launch modules to effect compressingly maintaining the plurality of launch modules in the launch orientation.
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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