Apparatus and methods for hypersonic nosecone

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United States of America Patent

PATENT NO 9297625
APP PUB NO 20150369576A1
SERIAL NO

14564024

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Abstract

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An apparatus and method for mitigating the shock front or reducing drag of a rocket or aerospace plane flying at hypersonic speeds by using a modified nose cone that incorporates a low temperature substance, such as liquid nitrogen, and where the nose cone simultaneously interacts with the ambient air to further supercool the nose cone during operation.

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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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