Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_68d07698f9dbdca32a84ab9ff36bfdfb |
classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08F291-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L5-00 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08F291-18 |
filingDate |
1958-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate |
1969-08-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1fa6aa7874e22ffa3ae8d650068361da |
publicationDate |
1969-08-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-3462952-A |
titleOfInvention |
Rocket propulsion process using irradiated solid polymeric propellant |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4981535-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5000803-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-6305286-B1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-3919011-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4986940-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5320692-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4278480-A http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2018170821-A1 |
priorityDate |
1958-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |