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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B23-00
filingDate 1988-02-03-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1989-01-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f65bc376765c765adaca51a844e8ada2
publicationDate 1989-01-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-4798636-A
titleOfInvention Composite solid propellant
abstract In order to achieve a stable burn characteristic, improved mechanical proties and reduced smoke development during burn, a composite solid propellant includes nitrides, borides, and carbonitrides of the metals zirconium, titanium, tungsten, hafnium, tantalum, or niobium as a burn moderator.
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priorityDate 1987-02-12-04:00^^<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: 34.