Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_20168ac7f1cf5ae83ae494e9666f5ad8 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42C19-0819 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-95 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42C19-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F42B3-11 |
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 |