http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2022157773-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_0a521cfa321c963978df8ae98a84056a |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B33-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B29-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L23-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06B23-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L47-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C06D5-00 |
| filingDate | 2021-03-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5e8bfbdfdd647407b7fa4a7353e81bb3 |
| publicationDate | 2022-10-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | JP-2022157773-A |
| titleOfInvention | Composite propellant |
| abstract | An object of the present invention is to provide a composite propellant having excellent manufacturability and good mechanical properties. In order to solve the above problems, a hydroxyl-terminated polybutadiene (HTPB), ammonium perchlorate (AP), and a phosphate are contained, and the content of the phosphate is 0.02 to 0.50. % by mass. According to the composite propellant of the present invention, a composite propellant having excellent manufacturability and good mechanical properties is provided by adding 0.02 to 0.50% by mass of a phosphate to the composite propellant. be able to. [Selection figure] None |
| priorityDate | 2021-03-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 76.