| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2f8cfa5aee4410611b5c562275c9f8e3 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C06B45-10 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B45-10 |
| filingDate |
1993-12-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cb3437100c83e1141df6bab9b7097e0e
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6ca4f571dba4fc332065c0a8ae21e3bf |
| publicationDate |
1995-06-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
JP-H07165483-A |
| titleOfInvention |
Gas generant composition |
| abstract |
(57) [Summary] [Objective] To provide a gas generant composition for use in rocket engines, propellants, etc., which is capable of controlling combustion speed and mechanical properties. [Structure] A terminal hydroxyl group-containing aliphatic polyether having an azide group in a side chain and an isocyanate-based curing agent are used, and the equivalent concentration ratio [NCO] / [OH] of the hydroxyl group and the isocyanate group is 0.5. A gas generant composition that is contained so as to be in the range of 1.0 or more and less than 1.0. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2017538648-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2012072007-A |
| priorityDate |
1993-12-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |