Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_87930e891c01680d2683bb261b1dc563 |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-70 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-70 |
filingDate |
1959-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate |
1963-05-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f34b894db7c692efdb4200646d63b9f6 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5e550da306c0f4e88ea7ac0c076d2973 |
publicationDate |
1963-05-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-3088274-A |
titleOfInvention |
Dual thrust rocket engine |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3471243-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-1264869-B http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3908364-A |
priorityDate |
1959-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |