http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-1241150-A2

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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-32
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-32
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B21-00
filingDate 2001-12-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_60e49b5112ab84a44d72480cf4c676dc
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_36002aeeb788d5f310fa664fcaa26ade
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_aa5c8f8d46360f301b38afd556cdb743
publicationDate 2002-09-18-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-1241150-A2
titleOfInvention Process for producing mouldable, plastic-bound explosives or rocket propellants
abstract The invention relates to a method for producing castable plastic-boundnExplosive charges or rocket fuels to which a metal powder is added, thenPowder grains have an essentially spherical shape.n n n In order to avoid that the viscosity of the explosive charge or the rocket fuel increases due to polar groups attached to the surface of the metal powder, the invention proposes that the polar groups of the metal powder be saturated by SiR 3 groups (Si = Silanes; R = organic residue). As a result, the polar groups can no longer react with the isocyanates of the explosive charge or the rocket fuel, and the specific surface area of the respective metal powder and the viscosity of the charges decrease.
priorityDate 2001-02-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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