Apparatus and methods for hypersonic stochastic switch

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United States of America Patent

PATENT NO 9550586
APP PUB NO 20160318634A1
SERIAL NO

15083128

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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 ensuing supercool/chilled air that is rendered as a consequence of supercooling may hence be compressed, regeneratively intercooled & flashed into liquid air. By means of extension, liquid air may be rendered as a direct result of said supercooling throughout the hypersonic regime into space. Also described are the details of an isentropically expanded hypersonic stochastic switch (a singularity), which is mainly achieved via the addition of a high pressure supersonic isentropic expansion nozzle whereby a continuous flow continuum is transformed into a stochastic flux.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Janeke, Charl E Los Angeles, US 19 137

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