http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5236152-A

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filingDate 1992-01-30-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1993-08-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e7a5515b8c1924e2c7a38ff35fbc4038
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publicationDate 1993-08-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-5236152-A
titleOfInvention Cooling/fuel system for hypersonic flight
abstract The present invention provides for the integration of structural cooling and fuel treatment within hypersonic vehicles. This is achieved by channeling a hydrocarbon fuel to a portion of the aircraft structure and imparting via the heat sink effect sufficient heat to cause a pyrolysis of the hydrocarbon fuel. After pyrolysis, the resulting fractions are then utilized as a fuel by the vehicle.
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priorityDate 1992-01-30-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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