Radiator systems
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United States of America Patent
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May 8, 2018
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app pub date -
Jul 27, 2016
filing date -
May 14, 2010
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Abstract
A system of spacecraft radiators comprising pre-formed thermal-transfer modules joined together by at least one solid-state welding process. Critical failure points are eliminated by forming the thermal-transfer modules as a single unitary piece, preferably by an extrusion process. The thermal-transfer modules allow the formation of larger radiator assemblies, which may comprise a wide range of sizes and physical geometries.
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