http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-4356870-B2
Outgoing Links
| Predicate | Object |
|---|---|
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-58 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-83 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C04B35-52 |
| filingDate | 2003-04-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2009-11-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2009-11-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-4356870-B2 |
| titleOfInvention | C / C composite manufacturing method, rocket nozzle and re-entry capsule |
| priorityDate | 2003-04-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 18.