A device for thermal monitoring a piece of equipment, which is integrated on a craft placed in a forced vacuum environment, an outside part of the equipment projecting outside of a wall of the craft and being subjected to a solar radiation flux, includes an absorbent screen that is suitable for being placed between the outside part of the equipment and the wall of the craft, whereby this absorbent screen has--on at least one portion of its front face, designed to be placed on the side removed from the wall of the craft--an absorptivity .alpha..sub.SOLAR that is the largest possible in the field of solar radiation, coupled to a low emissivity .epsilon..sub.IR in the infrared spectrum. The absorbent screen is made of a very heat-conductive material and has--on at least a portion of its rear face, suitable for being oriented toward the wall of the craft--a high emissivity .epsilon..sub.IR in the infrared spectrum, typically greater than or equal to 0.7.
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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