A payload cut-down mechanism having a pathway member having a first end and a second end attached to a balloon envelope, a line extending within the pathway member having first and second ends extending from the pathway member, where the first end of the line is releasably secured to a first actuated release mechanism attached to a payload, and a second end of the line releasably secured to a second actuated release mechanism attached to the payload, and wherein at least one of the first and second actuated release mechanisms are operable, upon receiving a signal, to release the first or second end of the line from one of the actuated release mechanisms and cause the payload to separate from the payload.
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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