http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3024594-A
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_9aa694d7d277529ddad12d81865f1b19 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-425 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06C9-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-42 |
filingDate | 1949-03-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 1962-03-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_59c0e8f2794adef8d4b12d6f17e6d9ed |
publicationDate | 1962-03-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | US-3024594-A |
titleOfInvention | Propellants for rocket motors |
priorityDate | 1949-03-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 32.