| Predicate |
Object |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B43-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-105
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B47-10 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B47-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B33-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B43-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64G1-00 |
| filingDate |
1989-07-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1993-04-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate |
1993-04-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
EP-0350135-B1 |
| titleOfInvention |
High-performance propellant combinations for a rocket engine |
| priorityDate |
1988-07-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |