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US Patent 11643930 Optics and structure for space applications

Patent 11643930 was granted and assigned to Trans Astronautica Corporation on May, 2023 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent
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Patent attributes

Patent Applicant
Trans Astronautica Corporation
Trans Astronautica Corporation
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Current Assignee
Trans Astronautica Corporation
Trans Astronautica Corporation
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
116439300
Patent Inventor Names
Joel C. Sercel0
Date of Patent
May 9, 2023
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Patent Application Number
176456710
Date Filed
December 22, 2021
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Patent Citations
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US Patent 11280194 Optics and structure for space applications
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US Patent 10654596 On-orbit thermal extractions of raw materials from space debris in support of additive manufacturing of new space elements on-orbit
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US Patent 10989443 Systems and methods for obtaining energy in shadowed regions
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US Patent 11085669 Optics and structure for space applications
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US Patent 11143026 Systems and methods for radiant gas dynamic mining of permafrost for propellant extraction
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US Patent 11391246 Omnivorous solar thermal thruster, cooling systems, and thermal energy transfer in rockets
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Patent Citations Received
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US Patent 12060172 Space object alert management and user interfaces
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US Patent 11987397 Systems and tagging interfaces for identification of space objects
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US Patent 12025006 Systems and methods for radiant gas dynamic mining of permafrost
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US Patent 12025078 Omnivorous solar thermal thruster, cooling systems, and thermal energy transfer in rockets
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Patent Primary Examiner
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Janine M Kreck
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CPC Code
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B64G 2001/224
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B64G 1/446
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B64G 1/22
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E21C 51/00
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A transportation network for providing propellant in space can include optical mining vehicles that concentrate solar energy to spall captured asteroids, capture released volatiles, and store them in reservoirs as propellants. The network can also have orbital transfer vehicles that use solar thermal rocket modules that focus solar energy on heat exchangers to force propellant through nozzles, as well as separable aeromaneuvering tanker modules with reusable heatshields and storage tanks. The network can have propellant depots positioned between Earth and a transport destination. The depots can mechanically couple to accept propellant delivery and to supply it to visiting space vehicles.

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