http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-1046626-B1

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filingDate 2000-04-14-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2004-08-18-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d2a76a3afcb651269c708a01a3d84c04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_92fbcb9cffcf7eb922eb17e2229d2921
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publicationDate 2004-08-18-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber EP-1046626-B1
titleOfInvention Rocket propellant
abstract Ammonium perchlorate-based fuel for low-smoke rocket propellant is surrounded by an inhibiting insulation layer comprising polyurethane binder and a mixture of 2-8 wt.% silicon carbide, 20-60 wt.% silicon dioxide and 2-20 wt.% heat-resistant carbon, polymer, silicate or ceramic fibers. Low-smoke rocket propellant, especially for end burners, comprises an ammonium perchlorate (AP)-based fuel containing an isocyanate-bonded, hydroxy-terminated polybutadiene binder, in which the fuel is surrounded by an inhibiting insulation layer comprising a polyurethane binder and a filler combination containing 2-8 wt.% silicon carbide, 20-60 wt.% silicon dioxide and 2- wt.% heat-resistant carbon, polymer, silicate or ceramic fibres with a length of 1-20 mm. An Independent claim is also included for a process for the production of rocket propellant by homogenizing the fillers and binder in a kneader and then processing the mixture to form the insulating layer by hardening the binder.
priorityDate 1999-04-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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