Superconductive Hypersonic Liquefaction Nosecone
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United States of America Patent
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Nov 24, 2015
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Aug 16, 2012
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Abstract
An apparatus and method for mitigating the shock front of a rocket or aerospace plane flying at hypersonic speeds while simultaneously distilling liquid chemical elements from the ambient air. The invention employs supercooling driven by the cryogenic power of liquid hydrogen and/or regenerative evaporation of liquid hydrogen and/or liquid nitrogen to drive isothermal compression and consequentially usurp the shock front in totality.
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