http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2893202-A
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_8857d9285f4a393618523d052bf765df |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B43-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-425 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B43-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-42 |
filingDate | 1953-12-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 1959-07-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f38956535e2869689f59d29f5475e263 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9b8db2f09ca6083a3c88c9380317e5ee |
publicationDate | 1959-07-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | US-2893202-A |
titleOfInvention | Rocket propulsion method |
priorityDate | 1953-12-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 37.