http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4874441-A

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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B33-08
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B33-08
filingDate 1988-12-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1989-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a876fcd00e4b00b40ecd984576d2e772
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_716f8e817181f8876d68d8001c74e8c5
publicationDate 1989-10-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-4874441-A
titleOfInvention Explosive for warheads and solid rocket propellant
abstract An explosive with maximum energy yield for warheads and solid rocket propellants comprises a high-energy secondary explosive with inorganic perchlorate and metal component with a high affinity for oxygen as well as desensitizing and binding agents. The oxygen balance sheet of the secondary explosive is balanced by the perchlorate component approximately to provide a complete reaction to give carbon dioxide and water. n Those explosive gases are reduced by the metal component, supplying energy, in accordance with the requirements made on the explosive.
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priorityDate 1988-01-05-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 33.