http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CA-1036419-A

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_20168ac7f1cf5ae83ae494e9666f5ad8
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06C9-00
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-95
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06C9-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42C19-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F42B3-11
filingDate 1975-08-25-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1978-08-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_78dd7bb8383f52137f52bf44682f24fe
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a27f3674cf1370757217bae8769954a5
publicationDate 1978-08-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CA-1036419-A
titleOfInvention Aft-end ignition system for rocket motor
abstract ABSTRACT An igniter for a rocket motor consisting of a cylindrical. tube having an open end and a closed end, a reduced section at the closed end, a plurality of segments extending outwardly from near the closed end, a squib secured in the reduced section, a charge in the tube and a polyurethane foam plug in the open end of the tube.
priorityDate 1975-08-25-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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Total number of triples: 25.