| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_926514a4805716ff3f04fdc6f91ab292 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08C19-34 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08C19-34 |
| filingDate |
1961-06-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
1971-07-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cb129dc1c4d6a437752ad5c4bfa4fe8c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b5b59629a1d79f4fab11e5615fbaecd4 |
| publicationDate |
1971-07-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-3595717-A |
| titleOfInvention |
Epoxy cured hydrocarbon polymer propellant composition and method of making the same |
| abstract |
1. A SOLID COMBUSTIBLE COMPOSITION ADAPTED TO BE USED AS A MISSILE PROPELLANT COMPRISING A DISPERSION OF A FINELY DIVIDED SOLID, NON-METALLIC, INORGANIC OXIDIZING AGENT IN A RUBBER-LIKE MATRIX HAVING A HIGH FUEL VALUE, SAID MATRIX BEING ESSENTIALLY AN EPOXIDE-CURED ACRYLOBUTADIENE COPOLYMER. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-5554820-A |
| priorityDate |
1961-06-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |